View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 07735U 26072.35601538 +.00000000 +00000-0 +10452-3 0 00008
2 07735 114.9736 27.4765 0054331 284.0785 75.4262 14.25570966 07
| Epoch (UTC): | 13 March 2026 08:32:39 |
| Eccentricity: | 0.0054331 |
| inclination: | 114.9736° |
| perigee height: | 768 km |
| apogee height: | 846 km |
| right ascension of ascending node: | 27.4765° |
| argument of perigee: | 284.0785° |
| revolutions per day: | 14.25570966 |
| mean anomaly at epoch: | 75.4262° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|