Progress manoeuvred successfully; new orbital vector

Agapov Vladimir (avm@kiam1.rssi.ru)
Wed, 20 Nov 1996 07:24:38 +0300

Both manoeuvres of Progress were successful. Here is EFG orbital vector
after processing of trajectory measurements on 4th orbit.

Orbit 4
20/11/1996
03:35:30.576 UTC
 3828.30229 km
-5459.26699 km
    0.00000 km
 3.50328728 km/s
 2.50664638 km/s
 6.06446071 km/s

nodal period     - 1h 30m 03.977s
semimaj. axis    - 6665.4830 km
eccentr.         - 0.005304018
inclin.          - 51.6749 deg
arg. of perig.   - 94.053056 deg
RAAN (B1950)     - 58.6069 deg
Hmin             - 255.18 km
Hmax             - 305.04 km

Best,
  Vladimir Agapov.