View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67371U 26145.46389686 +.00000000 +00000-0 +45360-3 0 00006
2 67371 97.8012 144.5534 0005443 189.6714 170.4399 14.89103409 03
| Epoch (UTC): | 25 May 2026 11:08:00 |
| Eccentricity: | 0.0005443 |
| inclination: | 97.8012° |
| perigee height: | 597 km |
| apogee height: | 605 km |
| right ascension of ascending node: | 144.5534° |
| argument of perigee: | 189.6714° |
| revolutions per day: | 14.89103409 |
| mean anomaly at epoch: | 170.4399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|