View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52675U 26145.47174514 +.00000000 +00000-0 +12916-3 0 00001
2 52675 53.2122 159.4346 0001332 102.3347 257.7795 15.08838236 09
| Epoch (UTC): | 25 May 2026 11:19:18 |
| Eccentricity: | 0.0001332 |
| inclination: | 53.2122° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.4346° |
| argument of perigee: | 102.3347° |
| revolutions per day: | 15.08838236 |
| mean anomaly at epoch: | 257.7795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|