View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20691U 26071.51825463 +.00000000 +00000-0 +24410-3 0 00005
2 20691 63.2940 112.4520 0882963 83.2941 286.7668 13.61987043 07
| Epoch (UTC): | 12 March 2026 12:26:17 |
| Eccentricity: | 0.0882963 |
| inclination: | 63.2940° |
| perigee height: | 375 km |
| apogee height: | 1682 km |
| right ascension of ascending node: | 112.4520° |
| argument of perigee: | 83.2941° |
| revolutions per day: | 13.61987043 |
| mean anomaly at epoch: | 286.7668° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|