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 25187.99319671 .00007695 00000-0 54190-3 0 9999
2 20682 63.2961 59.7944 0891517 76.2496 293.6061 13.60569400 56798
| Epoch (UTC): | 06 July 2025 23:50:12 |
| Eccentricity: | 0.0891517 |
| inclination: | 63.2961° |
| perigee height: | 373 km |
| apogee height: | 1694 km |
| right ascension of ascending node: | 59.7944° |
| argument of perigee: | 76.2496° |
| revolutions per day: | 13.60569400 |
| mean anomaly at epoch: | 293.6061° |
| orbit number at epoch: | 5679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|