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 24263.47090927 .00000574 00000-0 24751-3 0 9992
2 26931 67.0496 87.9528 0007641 266.9180 93.1047 14.31378482199446
| Epoch (UTC): | 19 September 2024 11:18:06 |
| Eccentricity: | 0.0007641 |
| inclination: | 67.0496° |
| perigee height: | 781 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 87.9528° |
| argument of perigee: | 266.9180° |
| revolutions per day: | 14.31378482 |
| mean anomaly at epoch: | 93.1047° |
| orbit number at epoch: | 19944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|