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 25341.74979015 .00000071 00000-0 11255-3 0 9993
2 00116 66.8104 359.2549 0070378 43.5819 317.0790 13.92286931270052
| Epoch (UTC): | 07 December 2025 17:59:41 |
| Eccentricity: | 0.0070378 |
| inclination: | 66.8104° |
| perigee height: | 869 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 359.2549° |
| argument of perigee: | 43.5819° |
| revolutions per day: | 13.92286931 |
| mean anomaly at epoch: | 317.0790° |
| orbit number at epoch: | 27005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|