View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26156.34226219 +.00000000 +00000-0 +16530-3 0 00005
2 20580 28.4714 161.5211 0001846 24.4267 335.6416 15.30618516 08
| Epoch (UTC): | 05 June 2026 08:12:51 |
| Eccentricity: | 0.0001846 |
| inclination: | 28.4714° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 161.5211° |
| argument of perigee: | 24.4267° |
| revolutions per day: | 15.30618516 |
| mean anomaly at epoch: | 335.6416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|