View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26561U 00061A 24005.50755753 .00009145 00000-0 38292-3 0 9991
2 26561 1.9514 346.9632 0013891 87.1832 272.9801 15.18347686276942
| Epoch (UTC): | 05 January 2024 12:10:52 |
| Eccentricity: | 0.0013891 |
| inclination: | 1.9514° |
| perigee height: | 501 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 346.9632° |
| argument of perigee: | 87.1832° |
| revolutions per day: | 15.18347686 |
| mean anomaly at epoch: | 272.9801° |
| orbit number at epoch: | 27694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|