View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63464U 26145.59480434 +.00000000 +00000-0 +74688-3 0 00007
2 63464 42.9998 185.8641 0001599 278.1935 81.8735 15.27586902 05
| Epoch (UTC): | 25 May 2026 14:16:31 |
| Eccentricity: | 0.0001599 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.8641° |
| argument of perigee: | 278.1935° |
| revolutions per day: | 15.27586902 |
| mean anomaly at epoch: | 81.8735° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|