View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66172U 26145.47083509 +.00000000 +00000-0 +67864-3 0 00003
2 66172 53.1571 66.1806 0000936 76.2199 283.8906 15.30210691 09
| Epoch (UTC): | 25 May 2026 11:18:00 |
| Eccentricity: | 0.0000936 |
| inclination: | 53.1571° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 66.1806° |
| argument of perigee: | 76.2199° |
| revolutions per day: | 15.30210691 |
| mean anomaly at epoch: | 283.8906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|