View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66595U 26144.90469161 +.00000000 +00000-0 +73688-3 0 00002
2 66595 43.0046 345.6118 0002246 261.9597 98.1000 15.27604615 06
| Epoch (UTC): | 24 May 2026 21:42:45 |
| Eccentricity: | 0.0002246 |
| inclination: | 43.0046° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 345.6118° |
| argument of perigee: | 261.9597° |
| revolutions per day: | 15.27604615 |
| mean anomaly at epoch: | 98.1000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|