View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20625U 26161.58595659 +.00000000 +00000-0 +18127-3 0 00008
2 20625 70.9988 102.8114 0013899 171.6308 188.5050 14.15023036 03
| Epoch (UTC): | 10 June 2026 14:03:46 |
| Eccentricity: | 0.0013899 |
| inclination: | 70.9988° |
| perigee height: | 832 km |
| apogee height: | 852 km |
| right ascension of ascending node: | 102.8114° |
| argument of perigee: | 171.6308° |
| revolutions per day: | 14.15023036 |
| mean anomaly at epoch: | 188.5050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|