View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56807U 26145.36934404 +.00000000 +00000-0 +32355-3 0 00001
2 56807 70.0000 130.9476 0003854 264.8809 95.1910 14.98332779 00
| Epoch (UTC): | 25 May 2026 08:51:51 |
| Eccentricity: | 0.0003854 |
| inclination: | 70.0000° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 130.9476° |
| argument of perigee: | 264.8809° |
| revolutions per day: | 14.98332779 |
| mean anomaly at epoch: | 95.1910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|