View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 51853C 22022B 24358.52687500 -.00001099 00000+0 -68946-4 0 3581
2 51853 53.2152 199.1906 0001354 89.0192 264.0959 15.08837436 10
| Epoch (UTC): | 23 December 2024 12:38:42 |
| Eccentricity: | 0.0001354 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 199.1906° |
| argument of perigee: | 89.0192° |
| revolutions per day: | 15.08837436 |
| mean anomaly at epoch: | 264.0959° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|