View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26022.21199640 +.00000000 +00000-0 +34472-3 0 00005
2 20580 28.4682 356.8795 0001648 319.5889 40.4584 15.28679599 08
| Epoch (UTC): | 22 January 2026 05:05:16 |
| Eccentricity: | 0.0001648 |
| inclination: | 28.4682° |
| perigee height: | 479 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 356.8795° |
| argument of perigee: | 319.5889° |
| revolutions per day: | 15.28679599 |
| mean anomaly at epoch: | 40.4584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|