View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66600U 26145.52657133 +.00000000 +00000-0 +85575-3 0 00004
2 66600 43.0034 342.5427 0001452 269.2945 90.7740 15.27615483 09
| Epoch (UTC): | 25 May 2026 12:38:15 |
| Eccentricity: | 0.0001452 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 342.5427° |
| argument of perigee: | 269.2945° |
| revolutions per day: | 15.27615483 |
| mean anomaly at epoch: | 90.7740° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|