View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59087U 26145.52041303 +.00000000 +00000-0 +77302-4 0 00001
2 59087 43.0021 236.6462 0001528 259.5015 100.5664 15.27581436 07
| Epoch (UTC): | 25 May 2026 12:29:23 |
| Eccentricity: | 0.0001528 |
| inclination: | 43.0021° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.6462° |
| argument of perigee: | 259.5015° |
| revolutions per day: | 15.27581436 |
| mean anomaly at epoch: | 100.5664° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|