View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00005U 58002B 24357.60320006 .00000410 00000-0 49256-3 0 9992
2 00005 34.2487 185.9078 1842632 216.6665 129.2724 10.85820623384402
| Epoch (UTC): | 22 December 2024 14:28:36 |
| Eccentricity: | 0.1842632 |
| inclination: | 34.2487° |
| perigee height: | 649 km |
| apogee height: | 3823 km |
| right ascension of ascending node: | 185.9078° |
| argument of perigee: | 216.6665° |
| revolutions per day: | 10.85820623 |
| mean anomaly at epoch: | 129.2724° |
| orbit number at epoch: | 38440 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|