View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32791U 08021J 23085.87883867 .00009640 00000-0 87312-3 0 9999
2 32791 97.6497 58.9471 0011207 339.3698 20.7069 14.95534211809435
| Epoch (UTC): | 26 March 2023 21:05:31 |
| Eccentricity: | 0.0011207 |
| inclination: | 97.6497° |
| perigee height: | 573 km |
| apogee height: | 588 km |
| right ascension of ascending node: | 58.9471° |
| argument of perigee: | 339.3698° |
| revolutions per day: | 14.95534211 |
| mean anomaly at epoch: | 20.7069° |
| orbit number at epoch: | 80943 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|