View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 31128U 07012M 25143.80750033 .00000853 00000-0 17019-3 0 9993
2 31128 98.3885 101.0736 0085986 213.0416 146.5396 14.62388444961418
| Epoch (UTC): | 23 May 2025 19:22:48 |
| Eccentricity: | 0.0085986 |
| inclination: | 98.3885° |
| perigee height: | 625 km |
| apogee height: | 746 km |
| right ascension of ascending node: | 101.0736° |
| argument of perigee: | 213.0416° |
| revolutions per day: | 14.62388444 |
| mean anomaly at epoch: | 146.5396° |
| orbit number at epoch: | 96141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|