View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 44404U 19038U 23033.45521181 .00021542 00000-0 91341-3 0 9990
2 44404 97.6610 10.8043 0019930 63.0391 297.2878 15.22963557197945
| Epoch (UTC): | 02 February 2023 10:55:30 |
| Eccentricity: | 0.0019930 |
| inclination: | 97.6610° |
| perigee height: | 483 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 10.8043° |
| argument of perigee: | 63.0391° |
| revolutions per day: | 15.22963557 |
| mean anomaly at epoch: | 297.2878° |
| orbit number at epoch: | 19794 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|