View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25336U 98029A 25093.51873396 0.00000000 00000-0 00000-0 0 01
2 25336 7.4121 352.7222 0038874 315.2961 44.2800 1.00270000 04
| Epoch (UTC): | 03 April 2025 12:26:58 |
| Eccentricity: | 0.0038874 |
| inclination: | 7.4121° |
| perigee height: | 35623 km |
| apogee height: | 35950 km |
| right ascension of ascending node: | 352.7222° |
| argument of perigee: | 315.2961° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 44.2800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|