F52 - User Spacecraft Mean Elements - Mitel GPS Orion-S/-HD Receiver User Manual

Document Title:
User's Manual for the GPS Orion-S/-HD Receiver
4.4.2.3 F52 – User Spacecraft Mean Elements
MsgID Chars. Format
F52 95
1 x
3 xxx
4 xxxx
11 xxxxxxx.xxx
11 xxxxxx.xxxx
11 xx.xxxxxxxx
9 xxxxx.xxxx
10 xxxxx.xxxx
10 xxxxx.xxxx
10 xxxxx.xxxx
12 xxx.xxxxxxxx
2 xx
1 x
Example:
<STX>F521079 475200.000
4397 -0.003070225C<ETX>
Document No.
GTN-MAN-0110
DLR/GSOCNo part of this document shall be reproduced in any form or disclosed to third parties without prior authorization.
Description
User spacecraft mean elements
<STX>
Message Id (=F52)
GPS week of epoch
GPS seconds of week [s] of epoch
SGP4 mean semi-major axis a [km]
SGP4 mean eccentricity e
SGP4 mean inclination i [deg]
SGP4 mean right ascension of ascending node
SGP4 mean argument of perigee
SGP4 mean mean anomaly M [deg]
SGP4 ballistic coefficient B
Checksum
<ETX>
6933.6698 0.00108870
[deg]
97.6045 143.0131 277.5609
42
[deg]
82.
Issue 1.0
June 22, 2003