View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67344U 26145.42953270 +.00000000 +00000-0 +55682-3 0 00006
2 67344 43.0013 153.3865 0002068 270.3217 89.7398 15.27593177 07
| Epoch (UTC): | 25 May 2026 10:18:31 |
| Eccentricity: | 0.0002068 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.3865° |
| argument of perigee: | 270.3217° |
| revolutions per day: | 15.27593177 |
| mean anomaly at epoch: | 89.7398° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|