View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38745U 26039.13724579 +.00000000 +00000-0 +10433-2 0 00001
2 38745 49.8265 118.9717 1611153 185.0144 173.2628 12.33967782 05
| Epoch (UTC): | 08 February 2026 03:17:38 |
| Eccentricity: | 0.1611153 |
| inclination: | 49.8265° |
| perigee height: | 258 km |
| apogee height: | 2807 km |
| right ascension of ascending node: | 118.9717° |
| argument of perigee: | 185.0144° |
| revolutions per day: | 12.33967782 |
| mean anomaly at epoch: | 173.2628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|