1999-064A
Control from Helios CMP at CNES/CST. Mass 2544 kg. Matra Marconi Space. Used Ariane medium fairing 02. The satellite failed in 2004.
| Helios 1B | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1999 Dec 3 | 1622:46 | Launch by Ariane 40 V124 | CSG ELA2 |
| T+2:56 Stage 1 sep | |||
| T+2:59 Stage 2 burn | |||
| T+3:45 Fairing 02 sep | |||
| T+5:13 Second stage sep | |||
| 1628 | T+5:18 Stage 3 (H10-3) burn | ||
| 1640:54 | T+18:08 Stage 3 MECO | ||
| 1641:06 | T+18:20 Helios 1B sep | ||
| 1644:39 | T+21:53 Clementine sep | ||
| 1999 Dec 5 | 98.00 660 x 666 x 98.1 | ||
| 1999 Dec | Orbit raising | ||
| 1999 Dec 15 | 98.37 679 x 681 x 98.1 | ||
| 2004 Sep 10 | 98.37 679 x 682 x 98.1 | ||
| 2004 Oct 14 | 98.37 679 x 681 x 98.15 | ||
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