View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00022U 59009A 24280.90180272 .00023115 00000-0 12115-2 0 9996
2 00022 50.2772 237.5042 0106073 184.3889 175.6145 15.10848963706276
| Epoch (UTC): | 06 October 2024 21:38:35 |
| Eccentricity: | 0.0106073 |
| inclination: | 50.2772° |
| perigee height: | 460 km |
| apogee height: | 607 km |
| right ascension of ascending node: | 237.5042° |
| argument of perigee: | 184.3889° |
| revolutions per day: | 15.10848963 |
| mean anomaly at epoch: | 175.6145° |
| orbit number at epoch: | 70627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|