View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00020U 59007A 23160.70728326 .00001194 00000-0 46722-3 0 9999
2 00020 33.3552 265.9596 1658908 278.3913 63.2766 11.57605483356461
| Epoch (UTC): | 09 June 2023 16:58:29 |
| Eccentricity: | 0.1658908 |
| inclination: | 33.3552° |
| perigee height: | 507 km |
| apogee height: | 3246 km |
| right ascension of ascending node: | 265.9596° |
| argument of perigee: | 278.3913° |
| revolutions per day: | 11.57605483 |
| mean anomaly at epoch: | 63.2766° |
| orbit number at epoch: | 35646 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|