View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20855U 26067.97259750 +.00000000 +00000-0 +10797-3 0 00005
2 20855 98.8224 51.4183 0024883 60.1009 7.4689 14.09160533 04
| Epoch (UTC): | 08 March 2026 23:20:32 |
| Eccentricity: | 0.0024883 |
| inclination: | 98.8224° |
| perigee height: | 844 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 51.4183° |
| argument of perigee: | 60.1009° |
| revolutions per day: | 14.09160533 |
| mean anomaly at epoch: | 7.4689° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|