View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20626U 26100.11729867 +.00000000 +00000-0 +73372-4 0 00005
2 20626 71.0180 339.5349 0207785 240.8560 274.2843 13.72950674 09
| Epoch (UTC): | 10 April 2026 02:48:54 |
| Eccentricity: | 0.0207785 |
| inclination: | 71.0180° |
| perigee height: | 836 km |
| apogee height: | 1142 km |
| right ascension of ascending node: | 339.5349° |
| argument of perigee: | 240.8560° |
| revolutions per day: | 13.72950674 |
| mean anomaly at epoch: | 274.2843° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|