View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 56995U 23084BX 24358.12130546 .00007589 00000-0 41967-3 0 9994
2 56995 97.7535 121.9689 0013238 250.3142 109.6661 15.14100014 84279
| Epoch (UTC): | 23 December 2024 02:54:40 |
| Eccentricity: | 0.0013238 |
| inclination: | 97.7535° |
| perigee height: | 514 km |
| apogee height: | 533 km |
| right ascension of ascending node: | 121.9689° |
| argument of perigee: | 250.3142° |
| revolutions per day: | 15.14100014 |
| mean anomaly at epoch: | 109.6661° |
| orbit number at epoch: | 8427 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|