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 23335.80880372 .00013438 00000-0 10968-2 0 9990
2 32791 97.6810 304.0107 0008993 192.6652 167.4347 14.99513621846832
| Epoch (UTC): | 01 December 2023 19:24:40 |
| Eccentricity: | 0.0008993 |
| inclination: | 97.6810° |
| perigee height: | 562 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 304.0107° |
| argument of perigee: | 192.6652° |
| revolutions per day: | 14.99513621 |
| mean anomaly at epoch: | 167.4347° |
| orbit number at epoch: | 84683 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|