View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26138.47583322 +.00000000 +00000-0 +14590-3 0 00004
2 20580 28.4751 283.5839 0001777 158.7414 201.3256 15.30412028 09
| Epoch (UTC): | 18 May 2026 11:25:11 |
| Eccentricity: | 0.0001777 |
| inclination: | 28.4751° |
| perigee height: | 473 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 283.5839° |
| argument of perigee: | 158.7414° |
| revolutions per day: | 15.30412028 |
| mean anomaly at epoch: | 201.3256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|