View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59415U 26145.23676257 +.00000000 +00000-0 +15651-3 0 00004
2 59415 43.0009 343.7872 0001355 276.2909 83.7788 15.27585625 02
| Epoch (UTC): | 25 May 2026 05:40:56 |
| Eccentricity: | 0.0001355 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 343.7872° |
| argument of perigee: | 276.2909° |
| revolutions per day: | 15.27585625 |
| mean anomaly at epoch: | 83.7788° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|