View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26153.34296605 +.00000000 +00000-0 +18209-3 0 00003
2 20580 28.4711 182.0162 0001701 354.7953 5.2625 15.30586461 04
| Epoch (UTC): | 02 June 2026 08:13:52 |
| Eccentricity: | 0.0001701 |
| inclination: | 28.4711° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 182.0162° |
| argument of perigee: | 354.7953° |
| revolutions per day: | 15.30586461 |
| mean anomaly at epoch: | 5.2625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|