View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66322U 26145.36725108 +.00000000 +00000-0 +63227-3 0 00005
2 66322 43.0028 139.2784 0001915 282.6903 77.3734 15.27590543 00
| Epoch (UTC): | 25 May 2026 08:48:50 |
| Eccentricity: | 0.0001915 |
| inclination: | 43.0028° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2784° |
| argument of perigee: | 282.6903° |
| revolutions per day: | 15.27590543 |
| mean anomaly at epoch: | 77.3734° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|