View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59666U 26145.21431102 +.00000000 +00000-0 +31762-4 0 00000
2 59666 43.0029 329.8802 0001265 270.8585 89.2121 15.27573283 09
| Epoch (UTC): | 25 May 2026 05:08:36 |
| Eccentricity: | 0.0001265 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 329.8802° |
| argument of perigee: | 270.8585° |
| revolutions per day: | 15.27573283 |
| mean anomaly at epoch: | 89.2121° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|