View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00116U 61015A 25340.81594496 .00000076 00000-0 11648-3 0 9997
2 00116 66.8105 1.5398 0070317 44.2862 316.3814 13.92286654269926
| Epoch (UTC): | 06 December 2025 19:34:57 |
| Eccentricity: | 0.0070317 |
| inclination: | 66.8105° |
| perigee height: | 869 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 1.5398° |
| argument of perigee: | 44.2862° |
| revolutions per day: | 13.92286654 |
| mean anomaly at epoch: | 316.3814° |
| orbit number at epoch: | 26992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|