View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66254U 26145.41859280 +.00000000 +00000-0 +54059-3 0 00007
2 66254 53.1588 287.5221 0001211 108.3504 251.7629 15.31731887 04
| Epoch (UTC): | 25 May 2026 10:02:46 |
| Eccentricity: | 0.0001211 |
| inclination: | 53.1588° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 287.5221° |
| argument of perigee: | 108.3504° |
| revolutions per day: | 15.31731887 |
| mean anomaly at epoch: | 251.7629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|