View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 61912U 24207A 25340.58601032 .00038704 00000-0 14073-2 0 9992
2 61912 42.9997 87.4936 0001103 271.3099 88.7626 15.27611394 61074
| Epoch (UTC): | 06 December 2025 14:03:51 |
| Eccentricity: | 0.0001103 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 87.4936° |
| argument of perigee: | 271.3099° |
| revolutions per day: | 15.27611394 |
| mean anomaly at epoch: | 88.7626° |
| orbit number at epoch: | 6107 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|