View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24727U 97006C 23083.96339550 .00000034 00000-0 12905-3 0 9997
2 24727 82.5998 285.8500 0000868 116.5246 0.6382 12.62340069202668
| Epoch (UTC): | 24 March 2023 23:07:17 |
| Eccentricity: | 0.0000868 |
| inclination: | 82.5998° |
| perigee height: | 1412 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 285.8500° |
| argument of perigee: | 116.5246° |
| revolutions per day: | 12.62340069 |
| mean anomaly at epoch: | 0.6382° |
| orbit number at epoch: | 20266 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|