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 23160.65068939 .00005798 00000-0 51276-3 0 9994
2 32791 97.6546 132.0453 0013630 79.6634 280.6124 14.96621317820538
| Epoch (UTC): | 09 June 2023 15:36:59 |
| Eccentricity: | 0.0013630 |
| inclination: | 97.6546° |
| perigee height: | 568 km |
| apogee height: | 587 km |
| right ascension of ascending node: | 132.0453° |
| argument of perigee: | 79.6634° |
| revolutions per day: | 14.96621317 |
| mean anomaly at epoch: | 280.6124° |
| orbit number at epoch: | 82053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|