View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66867U 26145.40231955 +.00000000 +00000-0 +71257-3 0 00008
2 66867 42.9982 270.5947 0001436 251.8878 108.1817 15.27601925 00
| Epoch (UTC): | 25 May 2026 09:39:20 |
| Eccentricity: | 0.0001436 |
| inclination: | 42.9982° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.5947° |
| argument of perigee: | 251.8878° |
| revolutions per day: | 15.27601925 |
| mean anomaly at epoch: | 108.1817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|