View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64338U 26144.93933913 +.00000000 +00000-0 +84892-3 0 00008
2 64338 42.9999 47.4693 0001529 251.3860 108.6826 15.27599016 09
| Epoch (UTC): | 24 May 2026 22:32:38 |
| Eccentricity: | 0.0001529 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 47.4693° |
| argument of perigee: | 251.3860° |
| revolutions per day: | 15.27599016 |
| mean anomaly at epoch: | 108.6826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|