View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65221U 26145.32496676 +.00000000 +00000-0 +90105-3 0 00008
2 65221 53.1583 156.0538 0001268 83.5855 276.5292 15.34407822 01
| Epoch (UTC): | 25 May 2026 07:47:57 |
| Eccentricity: | 0.0001268 |
| inclination: | 53.1583° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 156.0538° |
| argument of perigee: | 83.5855° |
| revolutions per day: | 15.34407822 |
| mean anomaly at epoch: | 276.5292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|