View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67331U 26145.02887829 +.00000000 +00000-0 +67836-3 0 00008
2 67331 43.0018 254.1709 0001990 283.4752 76.5878 15.27590018 05
| Epoch (UTC): | 25 May 2026 00:41:35 |
| Eccentricity: | 0.0001990 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.1709° |
| argument of perigee: | 283.4752° |
| revolutions per day: | 15.27590018 |
| mean anomaly at epoch: | 76.5878° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|