View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66417U 26145.65993271 +.00000000 +00000-0 +80637-4 0 00005
2 66417 50.0019 16.4267 0000868 54.6517 305.4436 13.29323587 05
| Epoch (UTC): | 25 May 2026 15:50:18 |
| Eccentricity: | 0.0000868 |
| inclination: | 50.0019° |
| perigee height: | 1149 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 16.4267° |
| argument of perigee: | 54.6517° |
| revolutions per day: | 13.29323587 |
| mean anomaly at epoch: | 305.4436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|