View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60923U 26144.78996980 +.00000000 +00000-0 -12018-5 0 00004
2 60923 53.1614 290.5463 0001204 95.8919 264.2219 15.30187590 04
| Epoch (UTC): | 24 May 2026 18:57:33 |
| Eccentricity: | 0.0001204 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 290.5463° |
| argument of perigee: | 95.8919° |
| revolutions per day: | 15.30187590 |
| mean anomaly at epoch: | 264.2219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|