View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20682U 26064.16176601 +.00000000 +00000-0 +43009-3 0 00006
2 20682 63.2953 129.3238 0879881 80.9220 289.0209 13.64464028 06
| Epoch (UTC): | 05 March 2026 03:52:56 |
| Eccentricity: | 0.0879881 |
| inclination: | 63.2953° |
| perigee height: | 369 km |
| apogee height: | 1670 km |
| right ascension of ascending node: | 129.3238° |
| argument of perigee: | 80.9220° |
| revolutions per day: | 13.64464028 |
| mean anomaly at epoch: | 289.0209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|