View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 06660U 73034B 23033.52360916 -.00000051 00000-0 -38910-4 0 9991
2 06660 81.2323 174.8568 0048177 72.9884 287.6556 14.05930503547053
| Epoch (UTC): | 02 February 2023 12:33:59 |
| Eccentricity: | 0.0048177 |
| inclination: | 81.2323° |
| perigee height: | 838 km |
| apogee height: | 908 km |
| right ascension of ascending node: | 174.8568° |
| argument of perigee: | 72.9884° |
| revolutions per day: | 14.05930503 |
| mean anomaly at epoch: | 287.6556° |
| orbit number at epoch: | 54705 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|