View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00107U 61013A 24254.63758899 .00006618 00000-0 82464-3 0 9999
2 00107 28.7907 59.3869 0516121 250.4630 103.9514 14.16599704184810
| Epoch (UTC): | 10 September 2024 15:18:07 |
| Eccentricity: | 0.0516121 |
| inclination: | 28.7907° |
| perigee height: | 464 km |
| apogee height: | 1209 km |
| right ascension of ascending node: | 59.3869° |
| argument of perigee: | 250.4630° |
| revolutions per day: | 14.16599704 |
| mean anomaly at epoch: | 103.9514° |
| orbit number at epoch: | 18481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|