View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 42759U 17034B 24337.50765090 .00044540 00000-0 10746-2 0 9990
2 42759 43.0150 347.9029 0012951 55.0785 305.1286 15.40413000413241
| Epoch (UTC): | 02 December 2024 12:11:01 |
| Eccentricity: | 0.0012951 |
| inclination: | 43.0150° |
| perigee height: | 436 km |
| apogee height: | 454 km |
| right ascension of ascending node: | 347.9029° |
| argument of perigee: | 55.0785° |
| revolutions per day: | 15.40413000 |
| mean anomaly at epoch: | 305.1286° |
| orbit number at epoch: | 41324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|