View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 07735U 75027B 25341.31596080 .00000193 00000-0 15462-3 0 9994
2 07735 114.9723 121.2630 0050048 308.4168 51.2427 14.25521989631123
| Epoch (UTC): | 07 December 2025 07:34:59 |
| Eccentricity: | 0.0050048 |
| inclination: | 114.9723° |
| perigee height: | 771 km |
| apogee height: | 843 km |
| right ascension of ascending node: | 121.2630° |
| argument of perigee: | 308.4168° |
| revolutions per day: | 14.25521989 |
| mean anomaly at epoch: | 51.2427° |
| orbit number at epoch: | 63112 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|