View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 53U 60009E 25168.02945785 -.00000072 00000-0 13765-3 0 9990
2 53 47.2790 28.7233 0100347 76.2103 284.9830 12.17384862890944
| Epoch (UTC): | 17 June 2025 00:42:25 |
| Eccentricity: | 0.0100347 |
| inclination: | 47.2790° |
| perigee height: | 1524 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 28.7233° |
| argument of perigee: | 76.2103° |
| revolutions per day: | 12.17384862 |
| mean anomaly at epoch: | 284.9830° |
| orbit number at epoch: | 89094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|