View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26286.62243497 +.00000000 +00000-0 +20260-3 0 00002
2 20580 28.4737 350.3749 0001899 43.5848 316.4898 15.31930979 04
| Epoch (UTC): | 13 October 2026 14:56:18 |
| Eccentricity: | 0.0001899 |
| inclination: | 28.4737° |
| perigee height: | 469 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 350.3749° |
| argument of perigee: | 43.5848° |
| revolutions per day: | 15.31930979 |
| mean anomaly at epoch: | 316.4898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|