View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 07560U 72062D 24357.04024965 .00000730 00000-0 41610-3 0 9991
2 07560 82.9755 224.4030 0067733 95.9363 264.9536 14.07268543563326
| Epoch (UTC): | 22 December 2024 00:57:57 |
| Eccentricity: | 0.0067733 |
| inclination: | 82.9755° |
| perigee height: | 819 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 224.4030° |
| argument of perigee: | 95.9363° |
| revolutions per day: | 14.07268543 |
| mean anomaly at epoch: | 264.9536° |
| orbit number at epoch: | 56332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|