View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 59281U 24052B 24277.15184297 .00001163 00000-0 53387-3 0 9997
2 59281 50.0102 137.7358 0004326 168.4004 191.7011 14.27642652 27735
| Epoch (UTC): | 03 October 2024 03:38:39 |
| Eccentricity: | 0.0004326 |
| inclination: | 50.0102° |
| perigee height: | 796 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 137.7358° |
| argument of perigee: | 168.4004° |
| revolutions per day: | 14.27642652 |
| mean anomaly at epoch: | 191.7011° |
| orbit number at epoch: | 2773 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|