View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43933U 19003B 22120.02431530 .22554430 23426-5 32043-2 0 9991
2 43933 97.1116 158.9235 0014855 252.7494 107.2177 16.34564232182763
| Epoch (UTC): | 30 April 2022 00:35:00 |
| Eccentricity: | 0.0014855 |
| inclination: | 97.1116° |
| perigee height: | 170 km |
| apogee height: | 190 km |
| right ascension of ascending node: | 158.9235° |
| argument of perigee: | 252.7494° |
| revolutions per day: | 16.34564232 |
| mean anomaly at epoch: | 107.2177° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|