View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 10514U 26099.99732353 +.00000000 +00000-0 +73017-4 0 00003
2 10514 81.2048 313.0130 0023810 165.1987 194.9887 14.11225242 08
| Epoch (UTC): | 09 April 2026 23:56:08 |
| Eccentricity: | 0.0023810 |
| inclination: | 81.2048° |
| perigee height: | 838 km |
| apogee height: | 872 km |
| right ascension of ascending node: | 313.0130° |
| argument of perigee: | 165.1987° |
| revolutions per day: | 14.11225242 |
| mean anomaly at epoch: | 194.9887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|