View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 31793U 26037.66806853 +.00000000 +00000-0 +25702-3 0 00005
2 31793 70.9731 237.5929 0001884 276.1934 147.8645 14.14829982 05
| Epoch (UTC): | 06 February 2026 16:02:01 |
| Eccentricity: | 0.0001884 |
| inclination: | 70.9731° |
| perigee height: | 842 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 237.5929° |
| argument of perigee: | 276.1934° |
| revolutions per day: | 14.14829982 |
| mean anomaly at epoch: | 147.8645° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|