View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64557U 26145.26869443 +.00000000 +00000-0 +15616-3 0 00002
2 64557 97.4691 260.7872 0002951 87.7484 272.4089 15.20275756 04
| Epoch (UTC): | 25 May 2026 06:26:55 |
| Eccentricity: | 0.0002951 |
| inclination: | 97.4691° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 260.7872° |
| argument of perigee: | 87.7484° |
| revolutions per day: | 15.20275756 |
| mean anomaly at epoch: | 272.4089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|