View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 04190U 69082BD 22141.33741357 .00010607 00000-0 13487-2 0 9991
2 04190 70.0300 9.1056 0027511 136.3636 223.9697 14.81551658768789
| Epoch (UTC): | 21 May 2022 08:05:52 |
| Eccentricity: | 0.0027511 |
| inclination: | 70.0300° |
| perigee height: | 605 km |
| apogee height: | 644 km |
| right ascension of ascending node: | 9.1056° |
| argument of perigee: | 136.3636° |
| revolutions per day: | 14.81551658 |
| mean anomaly at epoch: | 223.9697° |
| orbit number at epoch: | 76878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|