View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 21263U 26073.59246978 +.00000000 +00000-0 +75188-4 0 00008
2 21263 98.6158 63.5174 0012719 308.0314 51.9718 14.26719488 09
| Epoch (UTC): | 14 March 2026 14:13:09 |
| Eccentricity: | 0.0012719 |
| inclination: | 98.6158° |
| perigee height: | 794 km |
| apogee height: | 812 km |
| right ascension of ascending node: | 63.5174° |
| argument of perigee: | 308.0314° |
| revolutions per day: | 14.26719488 |
| mean anomaly at epoch: | 51.9718° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|