View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20625U 26066.78851096 +.00000000 +00000-0 -10216-3 0 00006
2 20625 70.9991 301.9077 0016214 302.1457 57.8092 14.15013122 06
| Epoch (UTC): | 07 March 2026 18:55:27 |
| Eccentricity: | 0.0016214 |
| inclination: | 70.9991° |
| perigee height: | 831 km |
| apogee height: | 854 km |
| right ascension of ascending node: | 301.9077° |
| argument of perigee: | 302.1457° |
| revolutions per day: | 14.15013122 |
| mean anomaly at epoch: | 57.8092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|