View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65934U 26145.45636358 +.00000000 +00000-0 +39349-3 0 00009
2 65934 53.1598 168.9441 0001244 84.3535 275.7608 15.30201759 00
| Epoch (UTC): | 25 May 2026 10:57:09 |
| Eccentricity: | 0.0001244 |
| inclination: | 53.1598° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 168.9441° |
| argument of perigee: | 84.3535° |
| revolutions per day: | 15.30201759 |
| mean anomaly at epoch: | 275.7608° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|