View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 20682U 90050B 25197.98840048 .00006761 00000-0 47629-3 0 9998
2 20682 63.2962 32.9161 0891206 76.4575 293.4058 13.60720517 58152
| Epoch (UTC): | 16 July 2025 23:43:17 |
| Eccentricity: | 0.0891206 |
| inclination: | 63.2962° |
| perigee height: | 372 km |
| apogee height: | 1693 km |
| right ascension of ascending node: | 32.9161° |
| argument of perigee: | 76.4575° |
| revolutions per day: | 13.60720517 |
| mean anomaly at epoch: | 293.4058° |
| orbit number at epoch: | 5815 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|