View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00694U 63047A 24286.42143049 .00004936 00000-0 60526-3 0 9992
2 00694 30.3578 177.7370 0561232 246.8368 107.2159 14.08738858 59095
| Epoch (UTC): | 12 October 2024 10:06:51 |
| Eccentricity: | 0.0561232 |
| inclination: | 30.3578° |
| perigee height: | 457 km |
| apogee height: | 1270 km |
| right ascension of ascending node: | 177.7370° |
| argument of perigee: | 246.8368° |
| revolutions per day: | 14.08738858 |
| mean anomaly at epoch: | 107.2159° |
| orbit number at epoch: | 5909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|