View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21153U 26065.33999294 +.00000000 +00000-0 +10183-3 0 00008
2 21153 82.9299 353.5609 0027657 253.8937 225.8175 13.76343655 01
| Epoch (UTC): | 06 March 2026 08:09:35 |
| Eccentricity: | 0.0027657 |
| inclination: | 82.9299° |
| perigee height: | 957 km |
| apogee height: | 997 km |
| right ascension of ascending node: | 353.5609° |
| argument of perigee: | 253.8937° |
| revolutions per day: | 13.76343655 |
| mean anomaly at epoch: | 225.8175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|