View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21891U 26064.57060884 +.00000000 +00000-0 +39390-3 0 00007
2 21891 19.9949 143.4576 0037902 281.2588 78.3575 14.93385812 08
| Epoch (UTC): | 05 March 2026 13:41:40 |
| Eccentricity: | 0.0037902 |
| inclination: | 19.9949° |
| perigee height: | 561 km |
| apogee height: | 614 km |
| right ascension of ascending node: | 143.4576° |
| argument of perigee: | 281.2588° |
| revolutions per day: | 14.93385812 |
| mean anomaly at epoch: | 78.3575° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|