1995-038A
The USA-113 payload was a DSCS III. The Lockheed Martin built satellite used an IABS upper stage, and for the first time an Atlas IIA launch vehicle. Mass of the satellite was 2689 kg including IABS. According to an Aviation Week report, the satellite was designated DSCS III B7 and was to be stationed over Indian Ocean.
| DSCS III (B7) | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1995 Jul 31 | 2330 | Launch by Atlas IIA | CC LC36A |
| 2332? | T+2:44? Atlas BECO | ||
| 2332? | T+2:47? Atlas sep | ||
| T+3:53? Fairing sep | |||
| T+4:41? Atlas SECO | |||
| 2334? | T+4:43? Atlas sep | ||
| 2335? | T+5:00? Centaur MES-1 | ||
| 2340? | T+10:07? Centaur MECO-1 | 158 x 893 x 29.4 (UN) | |
| 2352? | T+22:17? Centaur MES-2 | ||
| 2353? | T+23:43? Centaur MECO-2 | ||
| 2357 | T+26:38? Centaur sep | 228 x 35702 | |
| 1995 Aug 1 | 1600? | IABS burn 1 | |
| IABS sep | |||
| 1997 Oct | WLANT PRIME | GEO 52.5W | |
| 2003 Jan | GEO 148.5E | ||
| 2005 May | 1436.16 35760 x 35815 x 8.6 GEO 149.6E | ||
| 2005 Oct | 1436.12 35768 x 35805 x 8.5 GEO 179.6E | ||
| 2007 Jun | 1436.12 35749 x 35824 x 9.1 GEO 179.6E | ||
| 2012 Mar | 1436.10 35779 x 35794 x 9.7 GEO 103.8E | ||
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