View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00020U 59007A 24280.51499586 .00004393 00000-0 17636-2 0 9990
2 00020 33.3487 330.9903 1647456 341.8252 12.9598 11.59883126412697
| Epoch (UTC): | 06 October 2024 12:21:35 |
| Eccentricity: | 0.1647456 |
| inclination: | 33.3487° |
| perigee height: | 507 km |
| apogee height: | 3224 km |
| right ascension of ascending node: | 330.9903° |
| argument of perigee: | 341.8252° |
| revolutions per day: | 11.59883126 |
| mean anomaly at epoch: | 12.9598° |
| orbit number at epoch: | 41269 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|