View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 36596U 10027A 24282.51158889 .00030740 00000-0 20430-2 0 9997
2 36596 97.7683 278.0636 0009974 59.2912 300.9296 15.07083743781687
| Epoch (UTC): | 08 October 2024 12:16:41 |
| Eccentricity: | 0.0009974 |
| inclination: | 97.7683° |
| perigee height: | 538 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 278.0636° |
| argument of perigee: | 59.2912° |
| revolutions per day: | 15.07083743 |
| mean anomaly at epoch: | 300.9296° |
| orbit number at epoch: | 78168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|