View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20580U 26075.07602632 +.00000000 +00000-0 +21838-3 0 00009
2 20580 28.4725 356.4312 0001720 190.3932 169.6628 15.29590693 03
| Epoch (UTC): | 16 March 2026 01:49:28 |
| Eccentricity: | 0.0001720 |
| inclination: | 28.4725° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 356.4312° |
| argument of perigee: | 190.3932° |
| revolutions per day: | 15.29590693 |
| mean anomaly at epoch: | 169.6628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|