View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 20528U 26022.39399926 +.00000000 +00000-0 +67721-4 0 00009
2 20528 82.9343 262.3539 0030757 296.3464 237.5472 13.73146643 02
| Epoch (UTC): | 22 January 2026 09:27:21 |
| Eccentricity: | 0.0030757 |
| inclination: | 82.9343° |
| perigee height: | 966 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 262.3539° |
| argument of perigee: | 296.3464° |
| revolutions per day: | 13.73146643 |
| mean anomaly at epoch: | 237.5472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|