View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59602U 26145.54855100 +.00000000 +00000-0 +16647-4 0 00009
2 59602 43.0032 320.7025 0001714 267.3346 92.7310 15.27580231 05
| Epoch (UTC): | 25 May 2026 13:09:54 |
| Eccentricity: | 0.0001714 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.7025° |
| argument of perigee: | 267.3346° |
| revolutions per day: | 15.27580231 |
| mean anomaly at epoch: | 92.7310° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|