View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 25444U 26086.52776083 +.00000000 +00000-0 +48012-3 0 00000
2 25444 82.5518 264.4522 0016941 271.2867 147.1921 13.96983799 08
| Epoch (UTC): | 27 March 2026 12:39:58 |
| Eccentricity: | 0.0016941 |
| inclination: | 82.5518° |
| perigee height: | 892 km |
| apogee height: | 917 km |
| right ascension of ascending node: | 264.4522° |
| argument of perigee: | 271.2867° |
| revolutions per day: | 13.96983799 |
| mean anomaly at epoch: | 147.1921° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|