View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67927U 26145.39011612 +.00000000 +00000-0 +24586-3 0 00003
2 67927 43.0027 171.9838 0001495 276.8479 83.2203 15.27584715 01
| Epoch (UTC): | 25 May 2026 09:21:46 |
| Eccentricity: | 0.0001495 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 171.9838° |
| argument of perigee: | 276.8479° |
| revolutions per day: | 15.27584715 |
| mean anomaly at epoch: | 83.2203° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|