View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16262U 85108A 25340.66329645 .00033381 00000-0 69004-3 0 9994
2 16262 82.4625 58.6179 0005037 338.1536 21.9497 15.45644439187638
| Epoch (UTC): | 06 December 2025 15:55:08 |
| Eccentricity: | 0.0005037 |
| inclination: | 82.4625° |
| perigee height: | 426 km |
| apogee height: | 433 km |
| right ascension of ascending node: | 58.6179° |
| argument of perigee: | 338.1536° |
| revolutions per day: | 15.45644439 |
| mean anomaly at epoch: | 21.9497° |
| orbit number at epoch: | 18763 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|