View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29539U 06015F 22176.49948215 .00002682 00000-0 46117-3 0 9990
2 29539 97.9075 260.8937 0133124 94.7308 331.9657 14.63717950854900
| Epoch (UTC): | 25 June 2022 11:59:15 |
| Eccentricity: | 0.0133124 |
| inclination: | 97.9075° |
| perigee height: | 587 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 260.8937° |
| argument of perigee: | 94.7308° |
| revolutions per day: | 14.63717950 |
| mean anomaly at epoch: | 331.9657° |
| orbit number at epoch: | 85490 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|