Saturday, September 9, 2000

Transit T-3

 1976-089A


The final Transit Improvement Program satellite, TIP 3, suffered solar panel problems but was partially successful in its mission. Its orbit was raised between launch and Jan 1977 and then it was left to decay from its elliptical 450 x 868 km orbit.


TIP 3 
 

DateTimeEventOrbit  

1976 Sep 1  2114:02 Launch by Scout D-1  V SLC5 
 2115:23  T+1:21 St 1 burnout  -6293 x 60 x 77.7 
 2115:27 T+1:25 St 2 burn 
 2116:06 T+2:04 St 2 burnout  -5771 x 151 x 86.6  
 2116:17 T+2:15 Heatshield sep 
 2116:19 T+2:17 St 3 burn  
 2116:52 T+2:50 St 3 burnout 
 2121:48 T+7:46 Spin motors ignition 
 2121:50 T+7:48 St 3 sep 
 2121:55  T+7:53 St 4 burn  -4180 x 342 x 89.0 
 2122:29  T+8:27 St 4 burnout 342 x 869 x 90 (MOR) 
 2123?  St 4 sep 
   95.96 341 x 787 x 90.3 
1976 Oct 23    95.86 345 x 774 x 90.3 
1976 Oct 28   orbit raise 95.95 356 x 773 x 90.3 
1976 Nov 3   orbit raise 96.07 364 x 775 x 90.3 
1976 Dec 3   orbit raise  96.27 369 x 790 x 90.3 
1976 Dec 17   orbit raise  96.93 365 x 857 x 90.1 
1976 Dec 23    98.84 477 x 928 x 89.9 
1977 Jan 10    98.88 485 x 924 x 89.4 
1977 Jan 13   orbit lower 97.93 450 x 868 x 89.3 
1977 Mar end of ops? 
1977 May 3    97.90 451 x 864 x 89.3 
1979 Jul 28    96.81 440 x 771 x 89.3 
1981 May 29    88.21 169 x 202 x 89.3 
1981 May 30   Reentered 

DSCS-2 F7/8

 1979-098A


DSCS Phase 2 D-13 (satellite 9443) was launched with F-14 on 1979 Nov 21, a year after the sixth pair.


DSCS II D-13 
 

DateTimeEventOrbit  

1979 Nov 21  0209:36  Launch by Titan IIIC  CC LC40 
  T+1:50 St 1 burn 
  T+2:00? SRM sep 
  T+4:16 St 1 MECO 
  T+4:16 St 2 burn 
  T+5:00? Fairing sep
1979 Nov 21  0218  T+8 min Titan stage 2 sep  87.90 152 x 186 x 28.63  
 0315:00  Transtage MES-1 5:21 
 0320:21  Transtage MECO-1  150? x 35780? x 28? 
1979 Nov 21  0832? Transtage burn 2, 2min 1510.0 35818 x 38641 x 2.4 
 0834? Transtage MECO-2 
 0837  F-13 sep Transtage 
 0848  F-14 sep Transtage 
 0939?  F-13 despin 
1979 Nov 23    1431.24 35594 x 35788 x 2.4 GEO 90.5W+1.2E 
1979 Dec 5    1431.30 35594 x 35791 x 2.4 GEO 76.1W+1.2E 
1979 Dec 9   mv in for test 1436.24 35784 x 35794 x 2.4 GEO 77.9W 
1979 Dec 17   1436.27 35785 x 35794 x 2.4 GEO 78.2W 
1979 Dec 21   mv out  1429.73 35536 x 35787 x 2.4 GEO 66.9W+1.6E 
1979 Dec 30    1429.78 35537 x 35788 x 2.3 GEO 52.6W+1.6E 
1980 Jan 14   Braking 1435.09 35740 x 35793 x 2.4 GEO 15.3W+0.3E 
1980 Jan 25    1434.94 35734 x 35793 x 2.3 GEO 12.2W+0.3E 
1980 Jan 26   mv in  1436.16 35784 x 35791 x 2.3 GEO 12.3W 
1980 Jan 28   Operational, to DCA GEO 12W 
1980 Jun 4    1436.05 35771 x 35799 x 2.1 GEO 12.0W 
1980 Oct 12    1436.12 35776 x 35797 x 1.8 GEO 11.1W 
1981 Apr 26    1436.13 35781 x 35793 x 1.4 GEO 12.8W 
1981 Apr 30   mv out 1440.00 35785 x 35940 x 1.4 GEO 12.4W+1.0W 
1981 Aug 20    1440.25 35791 x 35943 x 1.1 GEO 126.0W+1.0W 
1981 Sep 5   mv in  1436.09 35778 x 35794 x 1.1 GEO 130.8W 
1982 Jan 6    1436.06 35776 x 35795 x 0.9 GEO 130.8W 
1982 Dec 11    1435.88 35773 x 35791 x 0.5 GEO 129.1W 
1983 Jan 2    1436.33 35786 x 35795 x 0.5 GEO 130.1W 
1983 Feb 13    1436.22 35781 x 35797 x 0.6 GEO 130.6W 
1983 Feb 14   mv out  1440.18 35792 x 35940 x 0.6 GEO 134.0W+1.0W 
1983 Apr 30   mv in  1436.14 35782 x 35792 x 0.7 GEO 179.7E 
1983 Jun 26    1435.90 35774 x 35791 x 0.8 GEO 179.1W 
1983 Jul   Move to 175E 
1983 Jul 26    1436.24 35785 x 35793 x 0.8 GEO 174.8E 
1984 Jan 2    1436.09 35781 x 35791 x 1.2 GEO 174.5E 
1985 Jan 19    1435.98 35776 x 35792 x 2.1 GEO 175.1E 
1986 Jan 6    1435.96 35780 x 35787 x 2.9 GEO 175.6E 
1987 Feb 2    1436.12 35783 x 35790 x 4.0 GEO 174.6E 
1989 Jan 4    1435.99 35777 x 35791 x 5.1 GEO 174.8E 
1989 Sep 27    1436.17 35778 x 35797 x 5.7 GEO 175.1E 
1989 Oct 3   mv out  1434.86 35744 x 35780 x 5.7 GEO 176.5E+0.3E 
1989 Oct 23   mv in  1436.03 35772 x 35798 x 5.8 GEO 179.3W 
1990 Apr 1    1435.97 35777 x 35791 x 6.2 GEO 179.2W 
1992 Feb 22    1436.09 35776 x 35796 x 7.8 GEO 179.8W 
1993 May 30    1436.10 35775 x 35798 x 8.9 GEO 179.8W 
1993 Jun 14    1436.06 35779 x 35792 x 8.9 GEO 179.8W 
1993 Jun 17   orbit raise  1444.97 35942 x 35977 x 8.9  
1993 Jun 17   orbit raise 1445.62 35954 x 35991 x 8.9 
1993 Jul 12   orbit raise 1451.39 36083 x 36088 x 9.0  
1993 Dec 1   orbit raise 1461.54 36273 x 36291 x 9.3 
1994 Jun 24   orbit raise 1493.02 36871 x 36915 x 9.7 
1994 Jul 19   orbit raise  1504.19 37096 x 37121 x 9.7 
1994 Aug 10    1506.20 37130 x 37165 x 9.8 

1979-098B

The DSCS II D-14 satellite (OPS 9444) was launched on 1979 Nov 21 with D-13.


DSCS II D-14 
 

DateTimeEventOrbit  

1979 Nov 21  2136  Launch by Titan IIIC  CC LC40 
1979 Nov 21  2144  Titan stage 2 sep 
1979 Nov 22  0359  Transtage burn 2  1510.0 
 0402  F-13 sep Transtage 
 0413  F-14 sep Transtage 
1979 Nov 23    1450.84 35791 x 36357 x 2.4 GEO 102.7W+3.6W 
1979 Dec 18   braking 1441.09 35791 x 35977 x 2.3 GEO 156.0W+1.2W 
1980 Feb 28    1441.00 35788 x 35977 x 2.1 GEO 117.0E+1.2W 
1980 Apr 30   mv in 1436.08 35784 x 35788 x 2.0 GEO 65.1E 
1980 Apr   Arr.IOR for comms with Gulf  GEO 66E 
1981 Mar 4    1435.96 35776 x 35792 x 1.3 GEO 65.6E 
1981 Mar   Move to 7W 
1981 Apr 2    1436.23 35773 x 35805 x 1.3 GEO 7.5W 
1981 Apr 30   mv out 1436.22 35776 x 35801 x 1.3 GEO 8.4W 
1981 May 12   mv in  1436.15 35783 x 35791 x 1.3 GEO 12.1W 
1981 Oct 5    1436.07 35774 x 35797 x 0.9 GEO 11.7W 
1982 Oct    GEO 12W 
1983 Jan 3    1436.06 35772 x 35799 x 0.4 GEO 12.6W 
1985 Apr 12    1436.12 35771 x 35802 x 2.3 GEO 12.2W 
1986 Mar 12    1436.10 35770 x 35802 x 3.2 GEO 12.2W 
1986 Mar 17   mv out  GEO 12W + 1/d 
1986 May 14   mv  GEO + 3/d 
1986 Jun 2    1447.86 35925 x 36107 x 3.4 GEO 126.1W+2.9W 
1986 Jun 21    GEO 180E 
1986 Aug 5    1436.08 35778 x 35793 x 3.5 GEO 179.1E 
1986 Oct    GEO 179W 
1987 Jul 26    1436.14 35782 x 35792 x 4.0 GEO 179.5E 
1988 Jan 3    1435.90 35773 x 35792 x 4.2 GEO 179.3W 
1989 Apr 15   1435.90 35777 x 35787 x 5.4 GEO 179.2W 
1989 May   Move to 174E 
1989 May 29    1436.08 35782 x 35790 x 5.5 GEO 174.2E 
1989 Oct 4    1436.02 35768 x 35801 x 5.8 GEO 174.7E 
1989 Oct 9   Move to 179W 
1989 Oct 31    1436.04 35767 x 35803 x 5.9 GEO 179.5W 
1990 Jan 3    1435.97 35771 x 35797 x 6.0 GEO 179.3W 
1990 Feb 12    1436.01 35775 x 35794 x 6.1 GEO 179.5E 
1990 Feb 18   move  1436.19 35780 x 35796 x 6.1 GEO 174.6E 
1990 Nov 15    1436.02 35779 x 35790 x 6.8 GEO 173.9E 
1990 Nov 26   mv out 1450.83 36063 x 36085 x 6.9 GEO 143.4E+3.6W 
1991 Jan 7   mv in  1436.18 35781 x 35795 x 6.9 GEO 63.9E 
1991 Mar 8    1436.18 35780 x 35795 x 7.1 GEO 65.0E 
1991 Oct 2    1436.15 35780 x 35795 x 7.6 GEO 65.4E 
1992 Sep 30    1436.09 35740 x 35832 x 8.4 GEO 64.8E 
1994 May 19    1435.92 35757 x 35809 x 9.7 GEO 66.0E 
1994 Jun 2   mv out  1435.90 35763 x 35802 x 9.7 GEO 66.6E+0.04E 
1994 Jul   IO ReserveGEO 72.0E 
1994 Oct 19   drift  1435.76 35765 x 35794 x 10.0 GEO 77.0E+0.08E 
1995 Apr 7    1436.11 35773 x 35800 x 10.3 GEO 84.7E+0.02E 
1995 Apr 17   Orbit raise 1442.48 35891 x 35931 x 10.3 GEO 72.4E+1.6W 
1995 Apr 20   Orbit raise 1448.76 36011 x 36057 x 10.3  
1995 Jun 12    1452.09 36074 x 36124 x 10.3 
1995 Jun 19   orbit raise  1463.92 36316 x 36342 x 10.4 
1995 Jul 26    1464.16 36315 x 36353 x 10.5 

Friday, September 8, 2000

Progress M-34

 1997-014A


Launch mass was 7156 kg. It carried at least two Orlan-M suits to Mir in Apr 1997. It was undocked in June and a redocking experiment using the TORU system was attempted, with disastrous results as the craft collided with the Spektr module.


Progress M-34 
 

DateTimeEventOrbit  

1997 Apr 6  1604:04.9  Launch by Soyuz-U  KB 
 1612:53.9  Blok-I sep 
 1941:45  TCM-1 
 2030:04  TCM-2 
1997 Apr 7  1656:16  TCM-3 
1997 Apr 8  1425:49  TCM-4
 1609:24  TCM-5

1730:03  Docked Kvant +X 
1997 Apr 15  1246:01  TCM raise Mir orbit 
1997 Jun 24 1022.50 Undocked Kvant +X 
1997 Jun 25  0700:52  TCM 1.5 m/s 
 0730:23  TCM 3.7 m/s 
 0841:47  TCM 1.7 m/s 

0902TORU manual control approach 
 0908:48 Braking 
 0909:51 Collided with Spektr module 
 0910:14  Second collision 
 0910?  Collisions with other modules 
 0918  TKG at 700m 
 0924:23  TORU shut off, TKG at 150m  
 0947  At 400m 
 1030  At 600m 
1997 Jun 28  0446:54  Test burn 1.7m/s 
 0923:00  Test burn 1.9 m/s 
1997 Jul 2  0534:58  Deorbit 86 m/s 205s burn 
 0614:50  Reentered over Pacific

Kosmos 2366

 1999-045A


Kosmos-2366 was a Parus satellite launched in 1999.


Kosmos-2366 
 

DateTimeEventOrbit  

1999 Aug 26  1202:15  Launch by Kosmos-3M  PL 
  T+2:10 St 1 MECO 
  T+2:12 St 1 sep 
 1204  T+2:12 St 2 burn 59km 
 1204  T+2:27 Fairing sep 76km 
 1210  T+8:03 St 2 MECO 150 km  150 x 1003? x 83 
 1304  T+1:02:19 St 2 MES2 
 1304  T+1:02:30 St 2 MECO2 
 1305  T+1:03 St 2 sep 
2000 Mar 15  104.84 963 x 1015 x 82.9 

DFH-5

  1975-119A


The second Feng Bao 1 launch to reach orbit carried another JSSW satellite, PRC 5.


JSSW 4 
 

DateTimeEventOrbit  

1975 Dec 16  0920  Launch by Feng Bao 1  JQ 
 0922  Stage 1 sep 
 0927? Stage 2 VECO 
 0927? Stage 2 sep  90.3 186 x 387 x 69.0 
1975 Dec 25    90.13 187 x 373 x 69.0 
1976 Apr 27   Reentered 

Kosmos 484

  1972-026A


Kosmos-484 was launched in Apr 1972 from Plesetsk. It carried a 5KS Nauka package to study electrons in the auroral zone and solar terrestrial interactions.


Kosmos-484 
 

DateTimeEventOrbit  

1972 Apr 6  0800:00 Launch by 11A57 PL 
 0804 Blok-I burn  
 0808 Blok-I sep  
 2107   88.64 193 x 221 x 81.2 
1972 Apr 7  0700   88.73 196 x 224 x 81.30 (RAE) 
1972 Apr 11  0306   88.54 190 x 213 x 81.3 
1972 Apr 18  0011   88.19 176 x 193 x 81.3 
1972 Apr 18   Capsule sep  
1972 Apr 18  0430? Retrofire 
 0440? PO sep 
 0445? Entry 
 0500? Landed after 11.86d 

Condition Critical

 https://welib.org/md5/2e95fb349c7f9478e0e172b2ad20c8be

Seventeen: April 2000

 https://welib.org/md5/dfa18c3fdf42d0a41359837e4c4abe6d

TDRS-4

 1989-021B


TDRS 4 (TDRS D before launch) was deployed from Discovery at 2112 on 1989 Mar 13, during mission STS-29R. The IUS burns were at 2209 on Mar 13 and 0324 on Mar 14, and a drift adjustment was made at 0700 on Mar 15. By 1989 Jun 10 TDRS 4 was on station replacing TDRS 1 as the TDRS EAST satellite at 41W.


TDRS 4 
 

DateTimeEventOrbit  

1989 Mar 13  1457:02  Launch from LC39B 
 1459:06  SRB sep 
 1500:39  80 km alt at 3:37 
 1505:30  MECO 110km  88.03 65 x 289 x 28.5 (PK) 
 1505:48  ET sep  88.18 72 x 296 x 28.5 (OMS dV) 
 1536:58  OMS-2 2:21 68m/s 
 1539:19  OMS-2 CO 
 1617  PLBD open  90.51 296 x 303 x 28.46 
 1927  ASE tilt 
 2110:12  TDRS deploy from OV-103 
 2210:12  IUS SRM-1 
 2212:38  SRM-1 burnout 
 2217:41  RCS-1 
 2218:01  RCS-1 off 
1989 Mar 14  
 0316:57  Exit cone extended 
 0322:37  SRM-1 sep 
 0324:15  SRM-2 burn 
 0326:04  IUS SRM-2 burnout 
 0329:45  RCS-2 
 0331:21 RCS-2 off 
 0341  TDRS solar arrays deploy 
 0404:58  SRM-2 sep 
 0410:44  SRM-2 CAM burn  
 0411:45  SRM-2 RCS depletion burn 
1989 Mar 14    1433.89 35647 x 35839 x 0.1 GEO 178.9W+0.5E 
1989 Mar 15  0700  mv, adjust drift 
1989 Mar 15    1433.68 35639 x 35838 x 0.1 GEO 178.6W+0.6E 
1989 Mar 21    1433.67 35618 x 35860 x 0.1 GEO 174.3W+0.6E 
1989 Apr 15   mv in tests 1435.90 35776 x 35788 x 0.2 GEO 149.8W 
1989 May 7    1435.81 35762 x 35799 x 0.2 GEO 148.7W 
1989 May   Mv out  
1989 May 20    1424.00 35529 x 35569 x 0.3 GEO 72.5W+3.0E 
1989 Jun 10   mv in 
1989 Jun 29   TDRS EAST 1435.99 35776 x 35792 x 0.4 GEO 40.7W 
1990 Oct 21    1436.24 35771 x 35807 x 0.4 GEO 41.2W 
1991 Jan 26    1436.02 35778 x 35792 x 0.7 GEO 40.9W 
1992 Sep 6    1436.13 35785 x 35788 x 0.0 GEO 41.0W 
1994 Apr 5    1436.10 35780 x 35792 x 0.0 GEO 41.0W 
1996 Feb 4    1436.08 35776 x 35795 x 0.0 GEO 41.0W 
1998 Apr 27    1436.14 35748 x 35826 x 1.3 GEO 41.0W

Spaceflight: February 2000

 https://welib.org/md5/840f6b1743233c69054a7729525c2198

Thursday, September 7, 2000

Intelsat 404

  1972-003A


The Intelsat IV F-4 satellite was the Pacific Primary satellite from 1972 to 1974.


Intelsat IV F-4 
 

DateTimeEventOrbit  

1972 Jan 23  0012  Launch by Atlas Centaur  CC LC36 
  T+2:32 BECO 
  T+2:35 Booster sep 
  T+3:17 Insulation panels 
  T+3:58 SECO, VECO  
 0016 T+4:01 Atlas sep 
  T+4:12 Centaur MES-1 
  T+4:24 Fairing 
 0022 T+10:18 Centaur MECO-1  190? x 1800? x 28? 
 0037 T+25:20 Centaur MES-2 
 0038 T+26:33 Centaur MECO-2 
 0040 T+28:47 Centaur sep 
1972 Jan 23   Centaur orbit  654.4 569 x 36610 x 28.4  
 0800?  Apo 1 over 70E 
 1900?  Apo 2 over 95W 
1972 Jan 24  0500?  Apo 3 over 103E 
 1600? Apo 4 over 60W 
1972 Jan 25  0300? Apo 5 over 140E 
 1400? Apo 6 over 25W 
1972 Jan 26  0030  Apo 7 over 170E 
1972 Jan 26  0032  AKM  GEO 165E dr 
1972 Feb 14   POR Primary, replaced III F4  GEO 174E 
1974 Dec   mv out  GEO 174E 
1975 Jan   POR Spare  GEO 179E 
1975 Dec 30    GEO 177.2E (Morgan) 
1977 Jan 2    1436.18 35671 x 35905 x 0.3 GEO 178.6E 
1978 Sep   POR Contingency  GEO 179E 
1980 Apr 9    1436.16 35783 x 35792 x 0.3 GEO 178.8E 
1981 Jun    GEO 179.0E+0.02, 0.0 
1982 Feb 23    1436.01 35772 x 35797 x 0.1 GEO 179.1E+0.0W 
1982 Feb 25   mv out  GEO 179E 
1982 Feb 27    1435.99 35742 x 35826 x 0.1 GEO 179.6E+0.0W 
1982 Mar 7    1435.95 35761 x 35805 x 0.1 GEO 179.7E+0.0W 
1982 Mar   mv out, AOR Spare  GEO 1W 
1982 Oct 7    1436.16 35778 x 35797 x 0.6 GEO 0.7W+0.0E 
1982 Oct   AOR spare  GEO 0W 
1983 Feb    GEO 0W 
1983 Feb 13    1436.18 35783 x 35793 x 0.9 GEO 1.2W+0.0E 
1983 Mar 14    1435.53 35772 x 35778 x 0.9 GEO 2.1E+0.1W 
1983 Mar   Decommissioned 1435.56 35774 x 35778 x 1.0 GEO 2.8E+0.1W
1983 Mar 30    1435.61 35774 x 35779 x 1.0 GEO 4.5E+0.1W 
1983 Apr 13    1436.62 35776 x 35817 x 1.0 GEO 6.7E+0.1E 
1983 May 4    1436.49 35765 x 35823 x 1.0 GEO 4.6E+0.1E 
1983 May 10   Orbit raise 
1983 May 16    1442.31 35900 x 35915 x 1.1 GEO 9.9W+1.6E 
1991 Apr 8    1442.52 35901 x 35922 x 8.3  
1993 Aug 15    1442.29 35903 x 35912 x 10.2 
1998 Jul 29    1442.32 35869 x 35946 x 12.9  

Hamptons Babylon : life among the super rich on America's Riviera

 https://welib.org/md5/01849f150e3c2c840e9f091837ea8054

Spaceflight: August 2000

 https://welib.org/md5/5bdb616b0ee2f0eb41c76eb48032fa69

Sunday, September 3, 2000

Himawari 4

 1989-070A


GMS 4 (Himawari 4) was launched by H-I from Tanageshima. Mass was 325 kg BOL after adapter separation. 3.4 high, 2.2 dia. Launch mass around 725 kg, AKM propellant 338 kg and hydrazine capacity 41 kg.

Stage 2 was intended to be marginally suborbital with an expected splash down at 1S 143W. GMS 4 was lighter than other H-I payloads and the launch vehicle had only 6 strapon boosters instead of the usual 9.


Himawari 4 
 

DateTimeEventOrbit  

1989 Sep 5  1911:00  Launch by H-I  TNSC 
 1912  Strapons sep (T+1:25) 
  T+4:27 MECO 
  T+4:33 VECO 
 1915  Stage 1 sep (T+4:38) 
  T+4:40 SES-2 
  T+5:36 Fairing sep
 1921  Stage 2 MECO 394 km (T+10:45)  -1630? x 550? x 30.7 ? 
   -2290? x 660? x 30.7?  
 1928  Apogee 
 1937 T+26:37 Spinup 
 1937 T+26:42 St 2 sep 
 1938 Stage 3 burn 62s (T+27:05) 354 km  
 1939  TECO T+28:07 
 1940  Stage 3 sep T+29:13  
 1940 T+29:09 Stage 3 tumble 
 1942  Stage 2 reentry 
1989 Sep 5    671.80 215 x 37846 x 28.6 
1989 Sep 6  0130?  Apo 1 
 0800?  Peri 1 
1989 Sep 6  1220:10  Apo 2, T+17:09 Star 27 AKM fired 
 1235? AKM ejected 
1989 Sep 8    1456.12 35258 x 37096 x 1.7 GEO 137.2E+4.9W 
1989 Sep 19    1422.55 35256 x 35785 x 1.2 
1989 Sep 22  0256 mv in
1989 Sep 22    1436.16 35719 x 35855 x 1.7 GEO 159.7E 
1989 Nov 9    1436.10 35722 x 35851 x 1.5 GEO 159.6E 
1989 Nov 15   mv out 
1989 Dec 4   Begin data 
1989 Dec 17   mv in  
1989 Dec 27    1436.03 35779 x 35791 x 1.4 GEO 139.9E 
1990 Jan 20    1436.15 35783 x 35791 x 1.4 GEO 139.9E 
1991 Jun 30    1436.03 35782 x 35788 x 0.4 GEO 140.1E 
1993 Oct 6    1436.19 35785 x 35790 x 0.0 GEO 140.1E 
1995 Jun 9    1436.16 35783 x 35792 x 1.0 GEO 139.7E 
1995 Jun 13   mv out 
1995 Aug 7   mv in  1436.12 35781 x 35792 x 1.2 GEO 120.0E 
1995 Oct 28    1436.06 35779 x 35792 x 1.3 GEO 120.4E 
1997 Aug 3    1436.10 35781 x 35791 x 2.6 GEO 120.2E 
1999 Jun 10    1436.00 35779 x 35789 x 3.9 GEO 120.0E

May 13,2026

  https://planet4589.org/space/jsr/back/news.855.txt