View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 28537U 05004A 26011.23965505 0.00000143 00000-0 10351-3 0 03
2 28537 63.3997 108.5862 0553234 3.9190 355.8652 13.41226746 08
| Epoch (UTC): | 11 January 2026 05:45:06 |
| Eccentricity: | 0.0553234 |
| inclination: | 63.3997° |
| perigee height: | 691 km |
| apogee height: | 1518 km |
| right ascension of ascending node: | 108.5862° |
| argument of perigee: | 3.9190° |
| revolutions per day: | 13.41226746 |
| mean anomaly at epoch: | 355.8652° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|