View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26131.88947560 +.00000000 +00000-0 +14321-3 0 00002
2 20580 28.4758 328.5711 0002189 94.3078 265.7768 15.30356852 08
| Epoch (UTC): | 11 May 2026 21:20:50 |
| Eccentricity: | 0.0002189 |
| inclination: | 28.4758° |
| perigee height: | 473 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 328.5711° |
| argument of perigee: | 94.3078° |
| revolutions per day: | 15.30356852 |
| mean anomaly at epoch: | 265.7768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|