View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59335U 26145.39220186 +.00000000 +00000-0 +39427-4 0 00006
2 59335 43.0018 113.5577 0001216 269.4612 90.6101 15.27579370 05
| Epoch (UTC): | 25 May 2026 09:24:46 |
| Eccentricity: | 0.0001216 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.5577° |
| argument of perigee: | 269.4612° |
| revolutions per day: | 15.27579370 |
| mean anomaly at epoch: | 90.6101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|