View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 31765U 99025CFQ 24358.03429208 .00164964 00000-0 20389-1 0 9990
2 31765 99.0632 200.4012 0079158 87.8092 65.6793 14.79680324890834
| Epoch (UTC): | 23 December 2024 00:49:22 |
| Eccentricity: | 0.0079158 |
| inclination: | 99.0632° |
| perigee height: | 575 km |
| apogee height: | 686 km |
| right ascension of ascending node: | 200.4012° |
| argument of perigee: | 87.8092° |
| revolutions per day: | 14.79680324 |
| mean anomaly at epoch: | 65.6793° |
| orbit number at epoch: | 89083 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|