View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28924U 26145.57614236 +.00000000 +00000-0 +00000-0 0 00000
2 28924 4.1648 76.7999 0006394 343.4614 204.2874 1.00272926 00
| Epoch (UTC): | 25 May 2026 13:49:38 |
| Eccentricity: | 0.0006394 |
| inclination: | 4.1648° |
| perigee height: | 35759 km |
| apogee height: | 35813 km |
| right ascension of ascending node: | 76.7999° |
| argument of perigee: | 343.4614° |
| revolutions per day: | 1.00272926 |
| mean anomaly at epoch: | 204.2874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|