View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26931U 01043C 24260.53621646 .00000737 00000-0 30901-3 0 9999
2 26931 67.0496 95.5368 0007651 267.2240 92.7986 14.31374250199182
| Epoch (UTC): | 16 September 2024 12:52:09 |
| Eccentricity: | 0.0007651 |
| inclination: | 67.0496° |
| perigee height: | 781 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 95.5368° |
| argument of perigee: | 267.2240° |
| revolutions per day: | 14.31374250 |
| mean anomaly at epoch: | 92.7986° |
| orbit number at epoch: | 19918 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|