View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 63264U 26145.42271699 +.00000000 +00000-0 +27338-3 0 00008
2 63264 97.6882 38.1707 0003238 78.7959 281.3627 14.97197542 08
| Epoch (UTC): | 25 May 2026 10:08:42 |
| Eccentricity: | 0.0003238 |
| inclination: | 97.6882° |
| perigee height: | 573 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 38.1707° |
| argument of perigee: | 78.7959° |
| revolutions per day: | 14.97197542 |
| mean anomaly at epoch: | 281.3627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|