View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28480U 04046B 25197.80759945 .00000103 00000-0 53035-4 0 9991
2 28480 98.1927 122.5326 0140569 132.0722 229.2518 14.26843467 74862
| Epoch (UTC): | 16 July 2025 19:22:56 |
| Eccentricity: | 0.0140569 |
| inclination: | 98.1927° |
| perigee height: | 701 km |
| apogee height: | 903 km |
| right ascension of ascending node: | 122.5326° |
| argument of perigee: | 132.0722° |
| revolutions per day: | 14.26843467 |
| mean anomaly at epoch: | 229.2518° |
| orbit number at epoch: | 7486 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|