View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28649U 05017A 24358.13855365 .00003565 00000-0 38844-3 0 9999
2 28649 97.5913 33.7663 0002560 76.3973 283.7530 14.88579273 63327
| Epoch (UTC): | 23 December 2024 03:19:31 |
| Eccentricity: | 0.0002560 |
| inclination: | 97.5913° |
| perigee height: | 600 km |
| apogee height: | 604 km |
| right ascension of ascending node: | 33.7663° |
| argument of perigee: | 76.3973° |
| revolutions per day: | 14.88579273 |
| mean anomaly at epoch: | 283.7530° |
| orbit number at epoch: | 6332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|