View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 07210U 74011B 24284.55805602 .00000390 00000-0 19520-3 0 9996
2 07210 81.2343 310.5463 0080025 338.1030 21.6728 14.13438532607157
| Epoch (UTC): | 10 October 2024 13:23:36 |
| Eccentricity: | 0.0080025 |
| inclination: | 81.2343° |
| perigee height: | 790 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 310.5463° |
| argument of perigee: | 338.1030° |
| revolutions per day: | 14.13438532 |
| mean anomaly at epoch: | 21.6728° |
| orbit number at epoch: | 60715 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|