View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20508U 26106.78490829 +.00000000 +00000-0 +47049-4 0 00008
2 20508 82.9524 119.3779 0042613 250.2896 283.2057 13.74552133 03
| Epoch (UTC): | 16 April 2026 18:50:16 |
| Eccentricity: | 0.0042613 |
| inclination: | 82.9524° |
| perigee height: | 952 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 119.3779° |
| argument of perigee: | 250.2896° |
| revolutions per day: | 13.74552133 |
| mean anomaly at epoch: | 283.2057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|