Tuesday, September 28, 1999
Transit O-25
1988-074A
The last of the four stacked Oscar launches, SOOS 4, included O-25 (NNS 30250).
| NNS O-25 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Aug 25 | 0659 | Launch by Scout | V SLC5 |
| T+1:18 St 1 burnout | -6318 x 83 x 74.9 | ||
| T+1:18 St 2 burn | |||
| T+1:59 St 2 burnout | |||
| T+2:03 Heatshield sep | -5951 x 298 x 85.7 | ||
| T+2:05 Stage 3 burn | |||
| T+3:53 Stage 3 burnout | |||
| 0711? | T+12:35? Stage 3 sep | ||
| 0711? | T+12:40 Stage 4 burn | -4601 x 1039 x 88.8 | |
| 0712 | T+13:14 Stage 4 burnout | ||
| 0713? | SOOS sep from Stage 4 | ||
| 0713? | Despin? | ||
| 0714? | SOOS upper sep from lower | ||
| 107.46 1034 x 1185 x 90.0 | |||
| 107.42 1035 x 1180 x 90.0 | |||
| 1988 Sep 3 | 1818 | To maintenance freq, storage | |
| 1990 Feb 9 | 1753 | Activated for tests | |
| 1990 Feb 14 | 1755 | Placed back in storage | |
| 1992 Dec 11 | 2038 | Placed in service | |
| 1993 May 18 | 2308 | In storage | |
| 1994 May 4 | 1537 | In service | |
| 1998 Jan | Still transmitting | ||
Saturday, September 18, 1999
MARECS 1
1981-122A
The MARECS program used the British Aerospace OTS/ECS comsat bus as a basis for a maritime communications satellite platform. MARECS A, known as MARECS 1 after launch, was launched in Dec 1981 on the fourth Ariane test flight.
| MARECS 1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1981 Dec 20 | 0129:00 | Launch by Ariane LO4 | CSG ELA1 |
| T+2:27 St 1 MECO | |||
| T+2:32 St 1 sep | |||
| T+2:32 L33 burn | |||
| T+4:13 Fairing | |||
| T+4:47 St 2 MECO | |||
| T+4:57 St 2 sep at 136 km | |||
| T+4:58 HM7 burn 9:11 | |||
| 0143:09 | T+14:09 HM7 MECO | ||
| T+15:20 spinup | |||
| 0144:40 | T+15:40 MARECS/CAT sep | ||
| 0145 | T+16m MARECS sep from CAT | ||
| 1981 Dec 21 | 631.94 219 x 35811 x 10.5 | ||
| 1981 Dec 21 | 1413:19 | Star 30 AKM 20s burn | |
| 1413:39 | AKM burnout | GEO 33.5W dr | |
| 1981 Dec 23 | 1430.72 35619 x 35742 x 2.3 GEO 33.7W+1.3E | ||
| 1982 Jan 2 | on station | GEO 26W | |
| 1982 Feb 10 | 1436.04 35774 x 35796 x 2.2 GEO 26.0W | ||
| 1982 Mar | INMARSAT Atlantic Primary, start ops | ||
| 1982 Jun | GEO 26W | ||
| 1985 Apr 26 | 1436.09 35773 x 35799 x 0.8 GEO 25.9W | ||
| 1986 Mar 3 | 1436.07 35771 x 35801 x 0.4 GEO 26.0W | ||
| 1986 Mar 5 | mv out | 1424.16 35536 x 35568 x 0.4 GEO 24.8W+3.0E | |
| 1986 Mar 10 | Drift W, replaced by MARECS 2 | ||
| 1986 May 12 | 1436.15 35764 x 35811 x 0.5 GEO 178.0E | ||
| 1986 Jun 9 | POR Spare | GEO 178E | |
| 1986 Oct 8 | GEO 178E | ||
| 1988 Jun 10 | 1436.12 35771 x 35802 x 2.3 GEO 177.8E | ||
| 1990 Aug 3 | 1436.08 35771 x 35801 x 4.2 GEO 178.0E | ||
| 1991 Mar 25 | Solar panel failure due to ESD | ||
| 1991 May 23 | 1436.09 35777 x 35795 x 4.2 GEO 178.0E | ||
| 1991 Jun | removed from active service | ||
| 1991 Jun | Replaced by MCS-D | ||
| 1991 Aug 29 | 1436.21 35772 x 35804 x 4.5 GEO 20.3E | ||
| 1991 Sep 30 | 1436.02 35769 x 35800 x 4.5 GEO 20.1E | ||
| 1992 Feb 9 | move to 22E | 1435.85 35769 x 35794 x 4.8 GEO 21.2E | |
| 1992 Mar 3 | mv in | 1435.74 35731 x 35827 x 4.9 GEO 22.5E | |
| 1994 Feb 24 | 1436.07 35773 x 35798 x 6.4 GEO 22.4E | ||
| 1996 Aug 16 | 1436.01 35728 x 35841 x 8.0 GEO 22.6E | ||
USA-122
1996-029D
USA 122 was launched into a 63 degree orbit by a Titan 4 in May 1996. Observers found the rocket body in a 312 x 622 km x 63.4 deg orbit, and later the triplet payloads were found in an 1150 km orbit. The SLDCOM ended up in a 2650 x 11600 km orbit.
| USA 122 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1996 May 12 | 2132 | Launch by Titan 403 | V SLC4E |
| 2134? | T+2:00 St 1 MES | ||
| 2134? | T+2:04 SRM sep | ||
| 2135? | T+3:59 Fairing sep | ||
| 2137? | T+5:09 St 2 MES | ||
| 2137? | T+5:10 St 1 sep | ||
| 2140? | T+8:50 St 2 MECO | ||
| 2141? | T+9m? Titan 4 stage 2 sep | ||
| Stage 2 sep | 312 x 622 x 63.4 (CSS) | ||
| 93.7 284 x 635 x 63.4 (UN) | |||
| 2324? | TLD burn 1 | 300 x 1100? | |
| 1996 May 13 | 0012? | TLD burn 2 | 1050 x 1150? |
| 1996 Jun 20 | 0739 | Deploy TIPS from host | |
| 1996 Jun 24? | Orbit raise burn | ||
| 1998 Jan 23 | 260.47 2653 x 11611 x 63.47 | ||
Vanguard 3
1959-007
The final Vanguard payload was the Magne-Ray satellite, a combined X-ray, meteoritic and magnetic field research satellite. The sphere was partly fiberglass and partly magnesium. It was the payload for TV4BU which for this last Vanguard flight carried a new third stage, the ABL X-248-A2, later known as Altair. The X-248 was similar to GCR's stage, but with a fiberglass casing instead of steel. It had the designation 38-DS-3100 and serial number SV-59. The new third stage increased payload mass by 13 kg, or velocity by 0.9 km/s for the standard payload mass. TV-4BU was informally called SLV-7, and the '7' was painted on the vehicle. Altair would become widely used on Scout and Delta. After a successful launch on 1959 Sep 18, the Magne-Ray payload became Vanguard III.
| Vanguard 3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1959 Sep 18 | 0520:07 | Launch by Vanguard SLV-7 | CC LC18A |
| 0522:32 | T+2:25 Stage 1 sep | |
| 0522:59 | T+2:52 Fairing sep | ||
| 0524:30 | T+4:22 Stage 2 burnout | ||
| 0528:59 | T+8:51 Stage 2 sep | -5325 x 505 x 33 | |
| 0529:13 | T+9:06 Stage 3 burn | ||
| 0529:25 | T+9:18 St 2 apogee 3.92 km/s, 505 km | ||
| 0529:49 | T+9:42 Stage 3 cutoff DV=4.39 km/s | 512 x 3744 x 33 | |
| Stage 2 impact 18 12N 56 45W | |||
| 1959 Dec 12 | End of transmissions | ||
Payload:
- Magnetometer
- Solar x-ray detector
Friday, September 17, 1999
USA-53
1990-019B
The AFP-731 satellite deployed by the Shuttle into a 65 degree orbit in Feb 1990 on mission STS-36 is believed to be a specialized imaging satellite. It's not clear whether it is related to the Improved CRYSTAL satellites. The satellite is reportedly called MISTY and was intended to be a low-observable `stealth' platform - but it was soon spotted by amateur observers.
The satellite was observed in a 257 x 270 km orbit at magnitude -1. On Mar 7 five debris objects, 1990-19C to G, were cataloged; although no orbital data were released, DoD reported that the objects would decay in a few months, and in July confirmed that they had done so. There were rumours that the fragments were an attempt to disguise a maneuver by the satellite. The main object was rediscovered, 3.5 mag fainter, by Russell Eberst and other observers on Oct 16, in an 800 km orbit. Working back the orbital precession confirmed that the new sighting was consistent with USA 53. The satellite was lost again in Nov 1990, just after a small orbital adjustment which may have been the precursor to a larger maneuver. It is believed the satellite may still be in a similar orbit.
| AFP-731 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1990 Feb 28 | 0750 | Launch by Shuttle | KSC LC39A |
| 1990 Mar 1 | 1845? | Deployed from OV-104 | 89.44 240 x 253 x 62.0 |
| 1990 Mar 3 | Small orbit correction | 89.78 257 x 270 x 62.0? | |
| 1990 Mar 7 | 5 debris objects cataloged | ||
| 1990 Mar 19 | one frag. decayed over Pacific | ||
| 1990 Mar 20? | 2nd frag. down | ||
| 1990 Apr-May | Remaining frags continue to decay | ||
| 1990 Jul 24 | DoD confirms all frag decayed | ||
| 1990 Oct 16 | Rediscovered by Eberst et al | 100.96 800 x 808 x 64.99 | |
| 1990 Oct 27 | 100.96 800 x 807 x 65.00 | ||
| 1990 Nov 2 ? | small orbit raise | ||
| 1990 Nov 5 | 100.96 797 x 811 x 65.02 | ||
| 1990 Nov | Orbit changed? | ||
Thursday, September 16, 1999
Nadezhda 3
1994-041A
The third named Nadezhda satellite was launched on 1994 Jul 14.
| Nadezhda 3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1994 Jul 14 | 0513:30 | Launch by Kosmos-3M | PL LC133 |
| T+2:10 St 1 MECO | |||
| T+2:12 St 1 sep | |||
| 0515 | T+2:12 St 2 burn 59km | ||
| 0515 | T+2:27 Fairing 76km | ||
| 0521 | T+8:03 St 2 MECO 150 km | 150 x 1003? x 83 | |
| 0615 | T+1:02:19 St 2 MES2 | ||
| 0615 | T+1:02:30 St 2 MECO2 | ||
| 0616? | T+1:02:50 St 2 sep | ||
| 1998 Jul | KOSPAS-7 decommissioned | ||
Sunday, September 12, 1999
Kosmos 361
1970-071A
Zenit-4M flight number 6 was launched three and a half hours after the landing of the fifth flight, the first time Zenit-4M missions were flown close together.
| Kosmos-361 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1970 Sep 8 | 1030:00 | Launch by 11A57 | PL |
| 1034 | Blok-I burn | ||
| 1038 | Blok-I sep | ||
| 1746 | 89.54 204 x 298 x 72.9 | ||
| 1970 Sep 9 | 0200 | 89.99 209 x 298 x 72.9 | |
| 1970 Sep 11 | 1725 | 89.51 203 x 296 x 72.9 | |
| 1970 Sep 12 | 2020 | Orbit raise | 90.04 230 x 322 x 72.9 |
| 1970 Sep 13 | 0500 | 90.09 203 x 353 x 72.9 (RAE) | |
| 1970 Sep 16 | 0956 | 90.03 202 x 349 x 72.9 | |
| 1970 Sep 20 | 0500? | Engine sep | |
| 1970 Sep 20 | 1429 | 89.98 200 x 347 x 72.9 | |
| 1970 Sep 21 | 0524? | Retrofire | |
| 0534? | PO sep | ||
| 0541? | Entry | ||
| 0554? | Landed after 12.8d | ||
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