|
View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line
orbital elements,
1 24034U 94029CF 99344.93607205 .05200752 00000-0 18320-1 0 8588
2 24034 81.9690 10.6228 0016312 82.3874 277.9246 15.85154936187293
| Epoch (UTC): | 10:27:57 PM, Friday, December 10, 1999 |
| Eccentricity: | 0.0016312 |
| Inclination: | 81.9690° |
| Perigee Height: | 305 km |
| Apogee Height: | 327 km |
| Right Ascension of Ascending Node: | 10.6228° |
| Argument of Perigee: | 82.3874° |
| Revolutions per Day: | 15.85154936 |
| Mean Anomaly at Epoch: | 277.9246° |
| Orbit Number at Epoch: | 18729 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
and the full part is where it is sunlit.
Developed and maintained by
Chris Peat, Heavens-Above GmbH
Please read the updated
FAQ before sending e-mail.
|
|
|
|
