View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64388U 26145.27258523 +.00000000 +00000-0 +62829-3 0 00004
2 64388 43.0015 106.9207 0001184 262.6389 97.4328 15.27596930 09
| Epoch (UTC): | 25 May 2026 06:32:31 |
| Eccentricity: | 0.0001184 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.9207° |
| argument of perigee: | 262.6389° |
| revolutions per day: | 15.27596930 |
| mean anomaly at epoch: | 97.4328° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|