View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 60382U 26145.60739631 +.00000000 +00000-0 +12782-3 0 00008
2 60382 88.9718 282.1490 0014878 80.5001 279.7831 13.51009436 09
| Epoch (UTC): | 25 May 2026 14:34:39 |
| Eccentricity: | 0.0014878 |
| inclination: | 88.9718° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 282.1490° |
| argument of perigee: | 80.5001° |
| revolutions per day: | 13.51009436 |
| mean anomaly at epoch: | 279.7831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|