View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65716U 26145.45681477 +.00000000 +00000-0 +21745-3 0 00000
2 65716 49.9866 53.5351 0009277 137.4358 222.7300 14.83284422 01
| Epoch (UTC): | 25 May 2026 10:57:48 |
| Eccentricity: | 0.0009277 |
| inclination: | 49.9866° |
| perigee height: | 612 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 53.5351° |
| argument of perigee: | 137.4358° |
| revolutions per day: | 14.83284422 |
| mean anomaly at epoch: | 222.7300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|