View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32785U 08021C 24280.85554946 .00020087 00000-0 16533-2 0 9995
2 32785 97.7690 245.4793 0008221 329.3935 30.6807 14.99107098892265
| Epoch (UTC): | 06 October 2024 20:31:59 |
| Eccentricity: | 0.0008221 |
| inclination: | 97.7690° |
| perigee height: | 564 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 245.4793° |
| argument of perigee: | 329.3935° |
| revolutions per day: | 14.99107098 |
| mean anomaly at epoch: | 30.6807° |
| orbit number at epoch: | 89226 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|