View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59605U 26145.53907631 +.00000000 +00000-0 +32730-4 0 00009
2 59605 43.0030 324.0896 0001002 278.2213 81.8525 15.27573577 05
| Epoch (UTC): | 25 May 2026 12:56:16 |
| Eccentricity: | 0.0001002 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.0896° |
| argument of perigee: | 278.2213° |
| revolutions per day: | 15.27573577 |
| mean anomaly at epoch: | 81.8525° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|