View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21937U 26032.24451138 +.00000000 +00000-0 +46643-4 0 00003
2 21937 82.9301 215.7517 0033523 169.0439 4.4831 13.73376749 03
| Epoch (UTC): | 01 February 2026 05:52:05 |
| Eccentricity: | 0.0033523 |
| inclination: | 82.9301° |
| perigee height: | 963 km |
| apogee height: | 1012 km |
| right ascension of ascending node: | 215.7517° |
| argument of perigee: | 169.0439° |
| revolutions per day: | 13.73376749 |
| mean anomaly at epoch: | 4.4831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|