View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16657U 86026C 24278.32642282 .00000285 00000-0 17699-2 0 9998
2 16657 7.0478 306.0288 7225167 99.5455 341.0727 2.25351857265934
| Epoch (UTC): | 04 October 2024 07:50:02 |
| Eccentricity: | 0.7225167 |
| inclination: | 7.0478° |
| perigee height: | 441 km |
| apogee height: | 35952 km |
| right ascension of ascending node: | 306.0288° |
| argument of perigee: | 99.5455° |
| revolutions per day: | 2.25351857 |
| mean anomaly at epoch: | 341.0727° |
| orbit number at epoch: | 26593 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|