View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 07727U 75025A 24357.45017676 -.00000010 00000-0 52899-4 0 9998
2 07727 65.5905 25.2897 0056608 356.6726 3.3962 13.99069481539907
| Epoch (UTC): | 22 December 2024 10:48:15 |
| Eccentricity: | 0.0056608 |
| inclination: | 65.5905° |
| perigee height: | 856 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 25.2897° |
| argument of perigee: | 356.6726° |
| revolutions per day: | 13.99069481 |
| mean anomaly at epoch: | 3.3962° |
| orbit number at epoch: | 53990 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|