View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66122U 26145.00362086 +.00000000 +00000-0 +61487-3 0 00002
2 66122 53.1585 45.2116 0001112 69.6903 290.4217 15.30208849 08
| Epoch (UTC): | 25 May 2026 00:05:12 |
| Eccentricity: | 0.0001112 |
| inclination: | 53.1585° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 45.2116° |
| argument of perigee: | 69.6903° |
| revolutions per day: | 15.30208849 |
| mean anomaly at epoch: | 290.4217° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|