View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59680U 26145.64633078 +.00000000 +00000-0 +35033-3 0 00003
2 59680 97.3247 221.5470 0014858 133.0588 227.1902 15.35210227 08
| Epoch (UTC): | 25 May 2026 15:30:42 |
| Eccentricity: | 0.0014858 |
| inclination: | 97.3247° |
| perigee height: | 450 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 221.5470° |
| argument of perigee: | 133.0588° |
| revolutions per day: | 15.35210227 |
| mean anomaly at epoch: | 227.1902° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|