View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 34810U 09020A 25358.93258989 0.00000000 00000-0 00000-0 0 06
2 34810 2.7881 81.1408 0004972 246.2147 113.7417 1.00270000 08
| Epoch (UTC): | 24 December 2025 22:22:55 |
| Eccentricity: | 0.0004972 |
| inclination: | 2.7881° |
| perigee height: | 35766 km |
| apogee height: | 35807 km |
| right ascension of ascending node: | 81.1408° |
| argument of perigee: | 246.2147° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 113.7417° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|