View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00692U 63039C 25231.55172954 -.00000605 00000-0 00000-0 0 9991
2 00692 27.9818 45.8257 5578653 215.3524 0.0919 0.22046177 12502
| Epoch (UTC): | 19 August 2025 13:14:29 |
| Eccentricity: | 0.5578653 |
| inclination: | 27.9818° |
| perigee height: | 44797 km |
| apogee height: | 173939 km |
| right ascension of ascending node: | 45.8257° |
| argument of perigee: | 215.3524° |
| revolutions per day: | 0.22046177 |
| mean anomaly at epoch: | 0.0919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|