View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39679U 14021B 24336.90796364 .00020640 00000-0 65299-3 0 9990
2 39679 51.6090 51.5724 0125876 233.0107 125.9296 15.25311390585312
| Epoch (UTC): | 01 December 2024 21:47:28 |
| Eccentricity: | 0.0125876 |
| inclination: | 51.6090° |
| perigee height: | 403 km |
| apogee height: | 576 km |
| right ascension of ascending node: | 51.5724° |
| argument of perigee: | 233.0107° |
| revolutions per day: | 15.25311390 |
| mean anomaly at epoch: | 125.9296° |
| orbit number at epoch: | 58531 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|