View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68223U 26145.38003807 +.00000000 +00000-0 +54940-3 0 00006
2 68223 97.2869 20.8666 0002014 91.5843 268.5630 15.33453827 00
| Epoch (UTC): | 25 May 2026 09:07:15 |
| Eccentricity: | 0.0002014 |
| inclination: | 97.2869° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8666° |
| argument of perigee: | 91.5843° |
| revolutions per day: | 15.33453827 |
| mean anomaly at epoch: | 268.5630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|