View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25867U 26105.90737653 +.00000000 +00000-0 +00000-0 0 00005
2 25867 55.1609 118.4976 7943121 310.5395 0.1381 0.37807016 00
| Epoch (UTC): | 15 April 2026 21:46:37 |
| Eccentricity: | 0.7943121 |
| inclination: | 55.1609° |
| perigee height: | 10239 km |
| apogee height: | 138583 km |
| right ascension of ascending node: | 118.4976° |
| argument of perigee: | 310.5395° |
| revolutions per day: | 0.37807016 |
| mean anomaly at epoch: | 0.1381° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|