View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66917U 26145.60539762 +.00000000 +00000-0 +44011-4 0 00002
2 66917 50.0022 227.0292 0001065 214.5040 145.5764 13.29325468 07
| Epoch (UTC): | 25 May 2026 14:31:46 |
| Eccentricity: | 0.0001065 |
| inclination: | 50.0022° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 227.0292° |
| argument of perigee: | 214.5040° |
| revolutions per day: | 13.29325468 |
| mean anomaly at epoch: | 145.5764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|