View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24007U 94029BC 24357.81697699 .00008161 00000-0 65619-3 0 9999
2 24007 81.9220 109.3940 0068727 238.2175 242.4978 14.98004695543689
| Epoch (UTC): | 22 December 2024 19:36:26 |
| Eccentricity: | 0.0068727 |
| inclination: | 81.9220° |
| perigee height: | 525 km |
| apogee height: | 621 km |
| right ascension of ascending node: | 109.3940° |
| argument of perigee: | 238.2175° |
| revolutions per day: | 14.98004695 |
| mean anomaly at epoch: | 242.4978° |
| orbit number at epoch: | 54368 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|