View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56523U 26145.44556367 +.00000000 +00000-0 +48311-4 0 00003
2 56523 43.0027 139.4143 0001571 277.7649 82.3024 15.27578217 04
| Epoch (UTC): | 25 May 2026 10:41:36 |
| Eccentricity: | 0.0001571 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.4143° |
| argument of perigee: | 277.7649° |
| revolutions per day: | 15.27578217 |
| mean anomaly at epoch: | 82.3024° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|