View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 15595U 85021A 23272.64331220 .00000466 00000-0 19596-3 0 9997
2 15595 108.0514 178.7353 0002322 294.8430 65.2470 14.38680869 20390
| Epoch (UTC): | 29 September 2023 15:26:22 |
| Eccentricity: | 0.0002322 |
| inclination: | 108.0514° |
| perigee height: | 761 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 178.7353° |
| argument of perigee: | 294.8430° |
| revolutions per day: | 14.38680869 |
| mean anomaly at epoch: | 65.2470° |
| orbit number at epoch: | 2039 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|