View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64189U 26145.12122546 +.00000000 +00000-0 +77627-3 0 00004
2 64189 53.1595 94.9389 0001191 82.7356 277.3782 15.34398572 06
| Epoch (UTC): | 25 May 2026 02:54:33 |
| Eccentricity: | 0.0001191 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 94.9389° |
| argument of perigee: | 82.7356° |
| revolutions per day: | 15.34398572 |
| mean anomaly at epoch: | 277.3782° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|