View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66605U 26145.58040534 +.00000000 +00000-0 +77053-3 0 00008
2 66605 43.0021 342.0797 0002889 287.4883 72.5653 15.27597578 08
| Epoch (UTC): | 25 May 2026 13:55:47 |
| Eccentricity: | 0.0002889 |
| inclination: | 43.0021° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 342.0797° |
| argument of perigee: | 287.4883° |
| revolutions per day: | 15.27597578 |
| mean anomaly at epoch: | 72.5653° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|