View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24278U 96046B 23333.44749379 .00000055 00000-0 93433-4 0 9995
2 24278 98.5551 289.6546 0350029 348.5184 10.8120 13.53164559347288
| Epoch (UTC): | 29 November 2023 10:44:23 |
| Eccentricity: | 0.0350029 |
| inclination: | 98.5551° |
| perigee height: | 800 km |
| apogee height: | 1321 km |
| right ascension of ascending node: | 289.6546° |
| argument of perigee: | 348.5184° |
| revolutions per day: | 13.53164559 |
| mean anomaly at epoch: | 10.8120° |
| orbit number at epoch: | 34728 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|