View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 39661U 26014.43796084 +.00000000 +00000-0 +14892-3 0 00009
2 39661 65.0080 78.3980 0014764 279.1857 80.7559 14.34496577 06
| Epoch (UTC): | 14 January 2026 10:30:39 |
| Eccentricity: | 0.0014764 |
| inclination: | 65.0080° |
| perigee height: | 766 km |
| apogee height: | 787 km |
| right ascension of ascending node: | 78.3980° |
| argument of perigee: | 279.1857° |
| revolutions per day: | 14.34496577 |
| mean anomaly at epoch: | 80.7559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|