NEWS

 
Asteroid 2005 YU Flyby
(Text and data from NASA)

NASA scientists will be tracking asteroid 2005 YU55 with antennas of the agency's Deep Space Network at Goldstone, Calif., as the space rock safely
flies past Earth slightly closer than the moon's orbit on Nov. 8. Scientists are treating the flyby of the 1,300-foot-wide (400-meter) asteroid as a
science target of opportunity - allowing instruments on "spacecraft Earth" to scan it during the close pass.
Tracking of the aircraft carrier-sized asteroid will begin at 9:30 a.m. local time (PDT) on Nov. 4, using the massive 70-meter (230-foot) Deep
Space Network antenna, and last for about two hours. The asteroid will continue to be tracked by Goldstone for at least four hours each day from
Nov. 6 through Nov. 10. Radar observations from the Arecibo Planetary Radar Facility in Puerto Rico will begin on Nov. 8, the same day the asteroid
will make its closest approach to Earth at 3:28 p.m. PST.
The trajectory of asteroid 2005 YU55 is well understood. At the point of closest approach, it will be no closer than 201,700 miles (324,600 kilometers)
or 0.85 the distance from the moon to Earth.  The gravitational influence of the asteroid will have no detectable effect on anything here on Earth,
including our planet's tides or tectonic plates. Although 2005 YU55 is in an orbit that regularly brings it to the vicinity of Earth (and Venus and
Mars), the 2011 encounter with Earth is the closest this space rock has come for at least the last 200 years.
During tracking, scientists will use the Goldstone and Arecibo antennas to bounce radio waves off the space rock. Radar echoes returned from 2005 YU55
will be collected and analyzed. NASA scientists hope to obtain images of the asteroid from Goldstone as fine as about 7 feet (2 meters) per pixel.
This should reveal a wealth of detail about the asteroid's surface features, shape, dimensions and other physical properties (see "Radar Love"
- http://www.jpl.nasa.gov/news/news.cfm?release=2006-00a ).
Arecibo radar observations of asteroid 2005 YU55 made in 2010 show it to be approximately spherical in shape. It is slowly spinning, with a rotation
period of about 18 hours. The asteroid's surface is darker than charcoal at optical wavelengths. Amateur astronomers who want to get a glimpse at YU55
will need a telescope with an aperture of 6 inches (15 centimeters) or larger.
The last time a space rock as big came as close to Earth was in 1976, although astronomers did not know about the flyby at the time. The next known
approach of an asteroid this large will be in 2028.
NASA detects, tracks and characterizes asteroids and comets passing close to Earth using both ground- and space-based telescopes. The Near-Earth
Object Observations Program, commonly called "Spaceguard," discovers these objects, characterizes a subset of them, and plots their orbits to determine
if any could be potentially hazardous to our planet.
NASA's Jet Propulsion Laboratory manages the Near-Earth Object Program Office for NASA's Science Mission Directorate in Washington. JPL is a division
of the California Institute of Technology in Pasadena.

Ephemerides

Date       UT    R.A. (J2000) Decl.    Delta     r     El.    Ph.   V      Sky Motion        Object    Sun   Moon
            h                                                              "/min    P.A.    Azi. Alt.  Alt.  Phase Dist. Alt.
2011 11 08 00   15 39 27.4 -13 06 35   0.0081  0.983   12.3 167.6  26.2   41.42    077.1    007  -57   -57   0.93   137  +36
2011 11 08 01   15 42 19.6 -12 57 00   0.0077  0.983   13.0 166.9  25.6   44.66    077.2    031  -54   -51   0.93   137  +26
2011 11 08 02   15 45 25.1 -12 46 41   0.0074  0.984   13.7 166.2  25.1   48.13    077.1    050  -47   -42   0.93   137  +16
2011 11 08 03   15 48 44.8 -12 35 28   0.0071  0.984   14.5 165.4  24.5   51.87    076.9    065  -38   -32   0.93   136  +06
2011 11 08 04   15 52 19.7 -12 23 10   0.0068  0.984   15.4 164.5  23.9   55.98    076.7    077  -29   -21   0.94   136  -03
2011 11 08 05   15 56 11.5 -12 09 35   0.0065  0.985   16.3 163.6  23.3   60.58    076.3    088  -19   -11   0.94   135  -13
2011 11 08 06   16 00 22.3 -11 54 26   0.0061  0.985   17.3 162.6  22.8   65.83    075.9    098  -09   -01   0.94   135  -21
2011 11 08 07   16 04 54.6 -11 37 24   0.0058  0.985   18.4 161.5  22.2   71.90    075.4    107  +00   +08   0.94   134  -27
2011 11 08 08   16 09 51.9 -11 18 04   0.0055  0.986   19.6 160.3  21.6   79.04    074.9    117  +10   +16   0.94   133  -31
2011 11 08 09   16 15 18.7 -10 55 59   0.0052  0.986   21.0 158.9  21.1   87.53    074.3    128  +18   +22   0.95   133  -33
2011 11 08 10   16 21 20.6 -10 30 34   0.0049  0.986   22.5 157.4  20.5   97.70    073.8    140  +25   +26   0.95   132  -31
2011 11 08 11   16 28 04.5 -10 01 07   0.0046  0.987   24.2 155.7  19.9  109.96    073.2    154  +30   +28   0.95   130  -27
2011 11 08 12   16 35 39.1 -09 26 49   0.0043  0.987   26.1 153.8  19.3  124.81    072.7    169  +34   +26   0.95   129  -21
2011 11 08 13   16 44 15.0 -08 46 38   0.0040  0.987   28.3 151.6  18.7  142.81    072.3    184  +35   +21   0.95   127  -13
2011 11 08 14   16 54 04.9 -07 59 23   0.0038  0.988   30.8 149.1  18.0  164.63    071.9    199  +34   +15   0.95   125  -04
2011 11 08 15   17 05 24.3 -07 03 33   0.0035  0.988   33.7 146.2  17.4  191.00    071.5    213  +31   +07   0.96   123  +06
2011 11 08 16   17 18 31.4 -05 57 26   0.0033  0.988   37.1 142.8  16.7  222.68    071.2    226  +27   -03   0.96   120  +16
2011 11 08 17   17 33 46.9 -04 39 04   0.0030  0.988   41.1 138.8  16.0  260.30    070.9    237  +22   -13   0.96   116  +27
2011 11 08 18   17 51 33.3 -03 06 26   0.0028  0.989   45.8 134.1  15.3  304.03    070.7    247  +17   -23   0.96   112  +37
2011 11 08 19   18 12 13.1 -01 17 47   0.0026  0.989   51.2 128.7  14.5  353.15    070.6    256  +12   -33   0.96   107  +45
2011 11 08 20   18 36 04.3 +00 47 35   0.0024  0.989   57.5 122.4  13.9  405.21    070.8    264  +07   -43   0.96   101  +53
2011 11 08 21   19 03 13.6 +03 08 23   0.0023  0.990   64.6 115.3  13.2  455.37    071.1    271  +03   -52   0.97   095  +57
2011 11 08 22   19 33 27.9 +05 40 10   0.0022  0.990   72.5 107.3  12.6  496.42    071.8    279  +00   -58   0.97   087  +57
2011 11 08 23   20 06 06.8 +08 14 55   0.0022  0.990   81.0  98.9  12.1  520.33    072.9    285  -03   -61   0.97   079  +52
2011 11 09 00   20 40 01.7 +10 42 21   0.0022  0.991   89.7  90.2  11.8  521.61    074.4    292  -06   -58   0.97   071  +45
2011 11 09 01   21 13 47.8 +12 52 46   0.0022  0.991   98.2  81.7  11.5  500.18    076.2    298  -08   -51   0.97   063  +36
2011 11 09 02   21 46 02.9 +14 40 04   0.0023  0.991  106.2  73.7  11.3  461.41    078.1    305  -11   -42   0.97   055  +26
2011 11 09 03   22 15 46.2 +16 02 49   0.0025  0.992  113.4  66.4  11.2  413.20    080.1    312  -14   -32   0.97   048  +16
2011 11 09 04   22 42 25.2 +17 03 19   0.0026  0.992  119.8  60.0  11.1  362.73    082.0    319  -17   -21   0.97   042  +06
2011 11 09 05   23 05 52.8 +17 45 42   0.0029  0.992  125.4  54.4  11.1  314.79    083.7    328  -20   -11   0.98   037  -03
2011 11 09 06   23 26 18.4 +18 14 21   0.0031  0.993  130.3  49.6  11.2  271.73    085.1    338  -23   -01   0.98   033  -12
2011 11 09 07   23 44 00.1 +18 33 03   0.0033  0.993  134.5  45.4  11.2  234.30    086.4    349  -25   +08   0.98   029  -19
2011 11 09 08   23 59 18.6 +18 44 48   0.0036  0.993  138.0  41.8  11.3  202.33    087.4    000  -25   +16   0.98   026  -25
2011 11 09 09   00 12 34.2 +18 51 46   0.0038  0.994  141.1  38.7  11.3  175.21    088.3    013  -24   +22   0.98   023  -28
2011 11 09 10   00 24 04.8 +18 55 31   0.0041  0.994  143.8  36.0  11.4  152.23    089.1    025  -21   +26   0.98   021  -29
2011 11 09 11   00 34 06.2 +18 57 05   0.0044  0.994  146.2  33.7  11.5  132.72    089.7    036  -17   +27   0.98   019  -27
2011 11 09 12   00 42 51.4 +18 57 12   0.0047  0.994  148.2  31.7  11.6  116.08    090.2    047  -11   +26   0.98   017  -22
2011 11 09 13   00 50 31.5 +18 56 20   0.0050  0.995  150.0  29.9  11.7  101.86    090.7    057  -04   +21   0.98   016  -16
2011 11 09 14   00 57 15.7 +18 54 46   0.0052  0.995  151.5  28.3  11.7   89.65    091.2    067  +04   +15   0.99   015  -07
2011 11 09 15   01 03 11.9 +18 52 43   0.0055  0.995  152.9  27.0  11.8   79.17    091.6    076  +13   +06   0.99   014  +02
2011 11 09 16   01 08 26.9 +18 50 17   0.0058  0.996  154.1  25.8  11.9   70.16    092.1    086  +23   -03   0.99   013  +12
2011 11 09 17   01 13 06.3 +18 47 32   0.0061  0.996  155.2  24.7  12.0   62.43    092.7    096  +32   -13   0.99   012  +22


*********************************************************************************************************


NASA’s decommissioned Upper Atmosphere Research Satellite fell back to Earth between 11:23 p.m.
EDT Friday, Sept. 23 and 1:09 a.m. EDT Sept. 24. The Joint Space Operations Center at Vandenberg
Air Force Base in California said the satellite penetrated the atmosphere over the Pacific Ocean.
The precise re-entry time and location are not yet known with certainty.


Updated 24 Sept. 05.00h UT
Crash date 24 September at 05.46h UT.

Updated 23 Sept. 20.55h UT
Crash date 24 September at 05.33h UT.

Updated 23 Sept. 19.30h UT
Crash date 24 September at 05.12h UT.

Updated 23 Sept. 19.00h UT
Crash date 24 September at 04.09h UT.

Updated 23 Sept. 14.30h UT
Crash date 24 September at 03.24h UT.

Updated 23 Sept. 11.30h UT
Crash date 24 September at 02.35h UT.

Updated 23 Sept. 08.30h UT
Orbit 129 x 132 km, crash date 24 September at 04.00h UT.

Updated 23 Sept. 07h UT
Orbit 129 x 132 km, crash date 24 September at 00.30h UT.

The orbit of UARS was 120 mi by 130 mi (190 km by 205 km). Re-entry is expected sometime during the afternoon of Sept. 23,
Eastern Daylight Time. The satellite will not be passing over North America during that time period. It is still too early
to predict the time and location of re-entry with any more certainty, but predictions will become more refined in the
next 24 to 48 hours.


Update 2

Reentry on 24 September 2011 at 02.28 UTC.

Update 1

Reentry on 23 September 2011 at 13 UTC.



US satellite may crash back to Earth Sept 23

WASHINGTON A 20-year-old satellite that measured the ozone layer is expected to crash back to Earth late next week,
but NASA said it still does not know where it will fall. The US space agency stressed that the risk to public safety
from the Upper Atmosphere Research Satellite (UARS) is "extremely small," and said that most, but not all, of the gear
will burn up on re-entry into Earth's atmosphere. "Re-entry is expected Sept. 23, plus or minus a day. The re-entry
of UARS is advancing because of a sharp increase in solar activity since the beginning of this week," NASA said in a
brief update on its website on Friday. "Safety is NASA's top priority," it added, noting that throughout history,
there have been "no confirmed reports of an injury resulting from re-entering space objects."
The decommissioned satellite could land anywhere between 57 degrees north latitude and 57 degrees south latitude,
a vast swath of populated territory. Predictions will only get more precise as the landing approaches.
The UARS satellite was sent into orbit in 1991 by the space shuttle Discovery.
The 35 by 15 foot (three by 10 meter) spacecraft weighed 13,000 pounds (5,900 kilograms) and toted 10 scientific
instruments for measuring wind, temperature and ozone chemistry. It was officially decommissioned in 2005.
"Although the spacecraft will break into pieces during re-entry, not all of it will burn up in the atmosphere," NASA said.
"It is impossible to pinpoint just where in that zone the debris will land, but NASA estimates the debris footprint
will be about 500 miles (800 kilometers) long," the space agency said.
It also urged anyone who comes across what they believe may be space debris not to touch it, but to call
authorities for assistance.



Asteroid Earth crossing at only 12000 kms from us

A little asteroid, with diameter of only 13 meter, will pass on June 27 (13:26 TDT) at 0.000123 A.U. from the Earth,
12000 kilometers from us.

2011 MD                                                  Earth MOID = 0.0006 AU
Epoch 2011 Aug. 27.0 TT = JDT 2455800.5                 MPC
M  51.54504              (2000.0)            P               Q
n   0.90091518     Peri.    6.12962     +0.15113548     +0.98754135
a   1.0617284      Node   272.56906     -0.90879587     +0.12137078
e   0.0431456      Incl.    2.51400     -0.38890632     +0.10015593
P   1.09           H   27.7

Data    TT       R. A. (2000)  Decl.      Delta       r     Elong.   Fase     V

2011 06 27.00   16 03 25.0   +27 29 10   0.001083  1.0171   119.3    60.7    15.1
2011 06 27.05   16 00 14.1   +26 26 25   0.001007  1.0171   119.6    60.3    14.9
2011 06 27.10   15 56 36.1   +25 13 00   0.000929  1.0170   120.1    59.9    14.7
2011 06 27.15   15 52 23.6   +23 45 38   0.000850  1.0170   120.5    59.4    14.5
2011 06 27.20   15 47 25.7   +21 59 27   0.000769  1.0170   121.1    58.9    14.3
2011 06 27.25   15 41 26.2   +19 46 54   0.000685  1.0169   121.7    58.3    14.0
2011 06 27.30   15 33 58.3   +16 55 28   0.000598  1.0169   122.4    57.6    13.7
2011 06 27.35   15 24 15.0   +13 02 42   0.000508  1.0169   123.2    56.8    13.3
2011 06 27.40   15 10 41.5   +07 23 40   0.000413  1.0168   123.9    56.1    12.9
2011 06 27.45   14 49 22.7   -01 47 17   0.000314  1.0168   124.0    56.0    12.3
2011 06 27.50   14 05 57.4   -19 38 26   0.000212  1.0167   120.5    59.5    11.5
2011 06 27.55   10 38 36.4   -57 13 48   0.000129  1.0166    96.5    83.5    11.2
2011 06 27.60   03 44 48.2   -21 01 03   0.000158  1.0165    58.9   121.1    13.7
2011 06 27.65   02 33 22.2   +08 40 08   0.000256  1.0165    56.9   123.0    14.9
2011 06 27.70   02 00 58.3   +21 30 35   0.000358  1.0164    60.3   119.7    15.3
2011 06 27.75   01 40 19.8   +28 33 29   0.000455  1.0164    63.1   116.8    15.6
2011 06 27.80   01 25 20.1   +33 03 02   0.000547  1.0164    65.3   114.7    15.9