View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 54699U 22169A 24358.39262375 .00000275 00000-0 16097-3 0 9992
2 54699 59.9948 227.3097 0018499 120.7032 239.5829 14.29204720106045
| Epoch (UTC): | 23 December 2024 09:25:22 |
| Eccentricity: | 0.0018499 |
| inclination: | 59.9948° |
| perigee height: | 781 km |
| apogee height: | 807 km |
| right ascension of ascending node: | 227.3097° |
| argument of perigee: | 120.7032° |
| revolutions per day: | 14.29204720 |
| mean anomaly at epoch: | 239.5829° |
| orbit number at epoch: | 10604 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|