View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 06139U 70025MV 22175.66170131 .00000850 00000-0 65204-3 0 9998
2 06139 99.0159 62.7162 0074614 24.9751 335.4991 13.94708589625885
| Epoch (UTC): | 24 June 2022 15:52:50 |
| Eccentricity: | 0.0074614 |
| inclination: | 99.0159° |
| perigee height: | 858 km |
| apogee height: | 966 km |
| right ascension of ascending node: | 62.7162° |
| argument of perigee: | 24.9751° |
| revolutions per day: | 13.94708589 |
| mean anomaly at epoch: | 335.4991° |
| orbit number at epoch: | 62588 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|