View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 06393U 73015B 25198.45694457 .00000014 00000-0 11435-5 0 9990
2 06393 81.2577 342.0646 0057237 261.7817 97.6858 14.05377234681312
| Epoch (UTC): | 17 July 2025 10:58:00 |
| Eccentricity: | 0.0057237 |
| inclination: | 81.2577° |
| perigee height: | 834 km |
| apogee height: | 917 km |
| right ascension of ascending node: | 342.0646° |
| argument of perigee: | 261.7817° |
| revolutions per day: | 14.05377234 |
| mean anomaly at epoch: | 97.6858° |
| orbit number at epoch: | 68131 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|