View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26265U 99057FB 23336.90107729 .00001865 00000-0 57197-3 0 9995
2 26265 98.7540 10.2557 0102072 86.7059 37.3503 14.39936709241170
| Epoch (UTC): | 02 December 2023 21:37:33 |
| Eccentricity: | 0.0102072 |
| inclination: | 98.7540° |
| perigee height: | 686 km |
| apogee height: | 831 km |
| right ascension of ascending node: | 10.2557° |
| argument of perigee: | 86.7059° |
| revolutions per day: | 14.39936709 |
| mean anomaly at epoch: | 37.3503° |
| orbit number at epoch: | 24117 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|