View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56780U 26145.44901198 +.00000000 +00000-0 +51269-4 0 00000
2 56780 69.9982 150.7155 0004274 267.9857 92.0812 14.98333385 05
| Epoch (UTC): | 25 May 2026 10:46:34 |
| Eccentricity: | 0.0004274 |
| inclination: | 69.9982° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 150.7155° |
| argument of perigee: | 267.9857° |
| revolutions per day: | 14.98333385 |
| mean anomaly at epoch: | 92.0812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|