View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20625U 26064.10222459 +.00000000 +00000-0 -83727-4 0 00003
2 20625 70.9998 307.5493 0016178 305.7503 54.2114 14.15014108 08
| Epoch (UTC): | 05 March 2026 02:27:12 |
| Eccentricity: | 0.0016178 |
| inclination: | 70.9998° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 307.5493° |
| argument of perigee: | 305.7503° |
| revolutions per day: | 14.15014108 |
| mean anomaly at epoch: | 54.2114° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|