View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66214U 26145.23381903 +.00000000 +00000-0 +68649-3 0 00005
2 66214 53.1602 234.7363 0001310 80.9389 279.1760 15.30211891 01
| Epoch (UTC): | 25 May 2026 05:36:41 |
| Eccentricity: | 0.0001310 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 234.7363° |
| argument of perigee: | 80.9389° |
| revolutions per day: | 15.30211891 |
| mean anomaly at epoch: | 279.1760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|