View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66388U 26145.21418579 +.00000000 +00000-0 +49000-3 0 00005
2 66388 53.1586 221.2979 0001324 85.8815 274.2337 15.30207836 01
| Epoch (UTC): | 25 May 2026 05:08:25 |
| Eccentricity: | 0.0001324 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 221.2979° |
| argument of perigee: | 85.8815° |
| revolutions per day: | 15.30207836 |
| mean anomaly at epoch: | 274.2337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|