View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 10974U 78067B 25312.78258617 .00000871 00000-0 88071-4 0 9990
2 10974 82.4791 142.0756 0015049 250.3126 109.6469 14.89817694542404
| Epoch (UTC): | 08 November 2025 18:46:55 |
| Eccentricity: | 0.0015049 |
| inclination: | 82.4791° |
| perigee height: | 588 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 142.0756° |
| argument of perigee: | 250.3126° |
| revolutions per day: | 14.89817694 |
| mean anomaly at epoch: | 109.6469° |
| orbit number at epoch: | 54240 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|