View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07734U 26087.78351494 +.00000000 +00000-0 +51828-4 0 00006
2 07734 114.9902 59.8741 0018915 305.6359 54.2958 14.19169968 05
| Epoch (UTC): | 28 March 2026 18:48:15 |
| Eccentricity: | 0.0018915 |
| inclination: | 114.9902° |
| perigee height: | 815 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 59.8741° |
| argument of perigee: | 305.6359° |
| revolutions per day: | 14.19169968 |
| mean anomaly at epoch: | 54.2958° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|