View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20671U 90057B 24284.46570479 .00000136 00000-0 10738-3 0 9991
2 20671 82.5485 47.8790 0015489 15.4191 344.7438 13.84697060732596
| Epoch (UTC): | 10 October 2024 11:10:36 |
| Eccentricity: | 0.0015489 |
| inclination: | 82.5485° |
| perigee height: | 936 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 47.8790° |
| argument of perigee: | 15.4191° |
| revolutions per day: | 13.84697060 |
| mean anomaly at epoch: | 344.7438° |
| orbit number at epoch: | 73259 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|