View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66088U 26145.27817955 +.00000000 +00000-0 +40279-3 0 00008
2 66088 53.1588 107.9144 0001340 80.1905 279.9247 15.30199765 03
| Epoch (UTC): | 25 May 2026 06:40:34 |
| Eccentricity: | 0.0001340 |
| inclination: | 53.1588° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 107.9144° |
| argument of perigee: | 80.1905° |
| revolutions per day: | 15.30199765 |
| mean anomaly at epoch: | 279.9247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|