View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21799U 26033.55360360 +.00000000 +00000-0 +35268-3 0 00000
2 21799 63.2968 145.8130 0885446 70.6120 298.8400 13.59871508 05
| Epoch (UTC): | 02 February 2026 13:17:11 |
| Eccentricity: | 0.0885446 |
| inclination: | 63.2968° |
| perigee height: | 380 km |
| apogee height: | 1693 km |
| right ascension of ascending node: | 145.8130° |
| argument of perigee: | 70.6120° |
| revolutions per day: | 13.59871508 |
| mean anomaly at epoch: | 298.8400° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|