View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 48908U 21059AF 24357.85758211 .00021315 00000-0 65978-3 0 9994
2 48908 97.6694 146.7914 0007099 132.2473 227.9372 15.33473120193667
| Epoch (UTC): | 22 December 2024 20:34:55 |
| Eccentricity: | 0.0007099 |
| inclination: | 97.6694° |
| perigee height: | 460 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 146.7914° |
| argument of perigee: | 132.2473° |
| revolutions per day: | 15.33473120 |
| mean anomaly at epoch: | 227.9372° |
| orbit number at epoch: | 19366 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|