View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66609U 26145.59839706 +.00000000 +00000-0 +47457-3 0 00005
2 66609 43.0026 342.2170 0001239 266.6619 93.4091 15.27587022 09
| Epoch (UTC): | 25 May 2026 14:21:41 |
| Eccentricity: | 0.0001239 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.2170° |
| argument of perigee: | 266.6619° |
| revolutions per day: | 15.27587022 |
| mean anomaly at epoch: | 93.4091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|