View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64668U 26145.23970588 +.00000000 +00000-0 +46549-3 0 00004
2 64668 53.1582 130.8121 0001130 82.5152 277.5979 15.34395801 05
| Epoch (UTC): | 25 May 2026 05:45:10 |
| Eccentricity: | 0.0001130 |
| inclination: | 53.1582° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.8121° |
| argument of perigee: | 82.5152° |
| revolutions per day: | 15.34395801 |
| mean anomaly at epoch: | 277.5979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|