View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66539U 26145.44628573 +.00000000 +00000-0 +63784-3 0 00000
2 66539 42.9981 204.3367 0001203 291.5845 68.4878 15.27592758 01
| Epoch (UTC): | 25 May 2026 10:42:39 |
| Eccentricity: | 0.0001203 |
| inclination: | 42.9981° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3367° |
| argument of perigee: | 291.5845° |
| revolutions per day: | 15.27592758 |
| mean anomaly at epoch: | 68.4878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|