View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68151U 26145.32881450 +.00000000 +00000-0 +80386-3 0 00001
2 68151 97.2850 166.9991 0002490 104.8983 255.2535 15.33488744 07
| Epoch (UTC): | 25 May 2026 07:53:29 |
| Eccentricity: | 0.0002490 |
| inclination: | 97.2850° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 166.9991° |
| argument of perigee: | 104.8983° |
| revolutions per day: | 15.33488744 |
| mean anomaly at epoch: | 255.2535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|