1996-070A
Lockheed Martin Telecommunications built the third Inmarsat III, this time with the usual apogee motor for Atlas launch from Canaveral. Mass was 2071 kg.
| Inmarsat III F3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1996 Dec 18 | 0157 | Launch by Atlas IIA AC-129 | CC LC36 |
| 0159 | Atlas booster sep | ||
| 0201 | Atlas sep | ||
| 0201 | Centaur MES-1 | ||
| 0207? | Centaur MECO-1 | 200? x 1045? x 28.5? | |
| 0222? | Centaur MES-2 | ||
| 0223? | Centaur MECO-2 | ||
| 0229 | Centaur sep T+32:02 | ||
| 1996 Dec 19 | 646.66 1007 x 35778 x 22.7 | ||
| 1996 Dec 20 | 0250? | AKM | |
| 1996 Dec 20 | 1429.48 35450 x 35863 x 2.7 GEO 154.8E+1.6E | ||
| 1996 Dec 27 | 1436.16 35698 x 35877 x 2.7 GEO 158.1E | ||
| 1997 Jan 15 | 1436.25 35694 x 35884 x 2.6 GEO 157.4E | ||
| 1997 Jan | mv out | ||
| 1997 Feb 1 | mv in | 1436.07 35768 x 35804 x 2.6 GEO 177.9E | |
| 1999 Oct 15 | 1436.05 35768 x 35802 x 0.6 GEO 178.1E | ||
| 2006 Aug 2 | 1436.10 35772 x 35800 x 0.0 GEO 178.1E | ||
No comments:
Post a Comment