View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 16409U 85119B 25198.44264629 .00000043 00000-0 25311-4 0 9999
2 16409 82.5377 168.9310 0015368 19.2833 340.8906 13.84909995999421
| Epoch (UTC): | 17 July 2025 10:37:24 |
| Eccentricity: | 0.0015368 |
| inclination: | 82.5377° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 168.9310° |
| argument of perigee: | 19.2833° |
| revolutions per day: | 13.84909995 |
| mean anomaly at epoch: | 340.8906° |
| orbit number at epoch: | 99942 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|