View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56374U 26145.38070441 +.00000000 +00000-0 +61545-5 0 00009
2 56374 43.0024 125.2078 0001068 270.4647 89.6082 15.27576179 03
| Epoch (UTC): | 25 May 2026 09:08:12 |
| Eccentricity: | 0.0001068 |
| inclination: | 43.0024° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 125.2078° |
| argument of perigee: | 270.4647° |
| revolutions per day: | 15.27576179 |
| mean anomaly at epoch: | 89.6082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|