2014-055A
This was a LM A2100 satellite on an Atlas V,with an imaging mission for the US government.
| CLIO | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2014 Sep 17 | 0010 | Launch by Atlas V 401 | CC SLC41 |
| T+4:02 BECO | |||
| T+4:08 St 1 sep | |||
| T+4:18 Centaur MES1 | |||
| T+4:25 PLF | |||
| 0027 | T+17:58 MECO-1 | 176 x 28871 x 27.91 | |
| 0257 | T+2:47:53 MES-2 | ||
| 0259 | T+2:49:03 MECO-2 | 11000? x 36000? x 20? | |
| 782.4 8461 x 35038 x 20.7 (UN) | |||
| 0301 | T+2:51:52 Centaur sep | ||
1996-020A
The Inmarsat III series carried L-band maritime communications payloads built by Matra Marconi Space UK. Mass of the satellite was 2068 kg launch, 1100 kg BOL, 860 kg dry. It replaced Inmarsat II F-1 as the IOR satellite at 64E.
| Inmarsat III G1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1996 Apr 3 | 2301:01 | Launch by Atlas IIA (AC-122) | CC LC36A |
| 2303 | BECO | ||
| 2303 | Booster sep | ||
| 2304 | Fairing sep | ||
| 2305 | SECO | ||
| 2305 | Atlas sep | ||
| 2306 | Centaur MES1 | ||
| 2311 | Centaur MECO-1 | ||
| 2323? | Centaur MES2 | ||
| 2325? | Centaur MECO2 | ||
| Centaur sep | |||
| 1996 Apr 3 | 642.95 1019 x 35577 x 21.9 | ||
| 1996 Apr 5 | 642.95 1020 x 35575 x 21.8 | ||
| 1996 Apr 6 | 1024? | AKM burn | |
| 1996 Apr 8 | 1414.5 35174 x 35549 x 2.7 | ||
| 1996 Apr 14 | 1436.01 35758 x 35811 x 2.7 GEO 27.6E | ||
| 1996 Apr 25 | 1435.96 35761 x 35806 x 2.6 GEO 27.8E | ||
| 1996 Apr 29 | mv out | ||
| 1996 May 3 | 1424.52 35546 x 35573 x 2.6 GEO 51.0E+3E | ||
| 1996 May 12 | 1436.11 35780 x 35793 x 2.6 GEO 63.9E | ||
| 1996 Sep 25 | 1436.04 35767 x 35803 x 2.4 GEO 64.1E | ||
| 1999 Oct 17 | 1436.09 35769 x 35803 x 0.1 GEO 63.9E | ||
| 2006 Aug 3 | 1436.06 35766 x 35805 x 0.0 GEO 63.7E | ||
| 2010 Dec 26 | 1436.10 35764 x 35809 x 0.1 GEO 64.5E | ||
| 2013 Jul 30 | 1436.09 35763 x 35809 x 1.2 GEO 64.4E | ||
