View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59406U 26144.96111122 +.00000000 +00000-0 +10591-4 0 00007
2 59406 43.0023 345.1619 0000989 255.4710 104.6032 15.27559239 01
| Epoch (UTC): | 24 May 2026 23:04:00 |
| Eccentricity: | 0.0000989 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.1619° |
| argument of perigee: | 255.4710° |
| revolutions per day: | 15.27559239 |
| mean anomaly at epoch: | 104.6032° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|