View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56965U 26059.12407981 +.00000000 +00000-0 +16146-3 0 00009
2 56965 97.5587 217.3641 0009709 247.4524 112.5754 16.50520813 07
| Epoch (UTC): | 28 February 2026 02:58:40 |
| Eccentricity: | 0.0009709 |
| inclination: | 97.5587° |
| perigee height: | 132 km |
| apogee height: | 144 km |
| right ascension of ascending node: | 217.3641° |
| argument of perigee: | 247.4524° |
| revolutions per day: | 16.50520813 |
| mean anomaly at epoch: | 112.5754° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|