View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56992U 23084BU 25042.76759540 .17342116 26494-5 33638-3 0 9995
2 56992 97.5047 178.6720 0014759 276.3055 83.6566 16.46134597 93271
| Epoch (UTC): | 11 February 2025 18:25:20 |
| Eccentricity: | 0.0014759 |
| inclination: | 97.5047° |
| perigee height: | 140 km |
| apogee height: | 159 km |
| right ascension of ascending node: | 178.6720° |
| argument of perigee: | 276.3055° |
| revolutions per day: | 16.46134597 |
| mean anomaly at epoch: | 83.6566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|