View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 10096U 77055B 25198.37315441 .00000461 00000-0 47320-4 0 9994
2 10096 75.8331 150.5016 0042036 240.2060 119.4949 14.91558308601684
| Epoch (UTC): | 17 July 2025 08:57:20 |
| Eccentricity: | 0.0042036 |
| inclination: | 75.8331° |
| perigee height: | 564 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 150.5016° |
| argument of perigee: | 240.2060° |
| revolutions per day: | 14.91558308 |
| mean anomaly at epoch: | 119.4949° |
| orbit number at epoch: | 60168 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|