When does the orbiter significantly change its orbit?

From: Walter Nissen (wnissen@tfn.net)
Date: Mon Aug 20 2001 - 16:03:21 PDT

  • Next message: Marek Kozubal: "RE: Satellite lunar transit" 

    Can anyone point to an explanation for the following, particularly how
one detects the time of the major impulses?  Or provide such an
explanation?

Thanks very much.

Walter Nissen

---

http://spaceflight.nasa.gov/realdata/sightings/SSapplications/Post/JavaS
SOP/orbit/SHUTTLE/SVPOST.html

IMPULSIVE TIG (GMT)   M50 DVx(FPS)      LVLH DVx(FPS)      DVmag(FPS)
IMPULSIVE TIG (MET)   M50 DVy(FPS)      LVLH DVy(FPS)      Invar Sph HA
DT                    M50 DVz(FPS)      LVLH DVz(FPS)      Invar Sph HP

-

232/16:11:26.402           0.5              -6.0              6.0
009/19:01:12.420          -5.1               0.0              218.9
000/00:00:24.839           3.0               0.1              205.4

232/20:40:21.863          -3.6             -11.0              11.0
009/23:30:07.880          -6.3              -0.0              218.5
000/00:00:15.761           8.2               0.1              199.7

-----------------------------------------------------------------
Unsubscribe from SeeSat-L by sending a message with 'unsubscribe'
in the SUBJECT to SeeSat-L-request@lists.satellite.eu.org
http://www2.satellite.eu.org/seesat/seesatindex.html

    This archive was generated by hypermail 2b29 : Mon Aug 20 2001 - 15:30:30 PDT