View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 59790U 26145.43054205 +.00000000 +00000-0 +34100-4 0 00006
2 59790 43.0033 135.3599 0001612 285.0657 75.0016 15.27579003 01
| Epoch (UTC): | 25 May 2026 10:19:58 |
| Eccentricity: | 0.0001612 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.3599° |
| argument of perigee: | 285.0657° |
| revolutions per day: | 15.27579003 |
| mean anomaly at epoch: | 75.0016° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|