View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24827U 97028A 24357.62973053 -.00000170 00000-0 -13524-2 0 9992
2 24827 63.3103 34.3386 1079449 62.5488 94.9349 11.07965692114555
| Epoch (UTC): | 22 December 2024 15:06:48 |
| Eccentricity: | 0.1079449 |
| inclination: | 63.3103° |
| perigee height: | 1204 km |
| apogee height: | 3038 km |
| right ascension of ascending node: | 34.3386° |
| argument of perigee: | 62.5488° |
| revolutions per day: | 11.07965692 |
| mean anomaly at epoch: | 94.9349° |
| orbit number at epoch: | 11455 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|