View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 57627U 26145.60106041 +.00000000 +00000-0 +17480-3 0 00009
2 57627 45.0034 56.1266 0004605 155.9444 204.1629 14.61536139 01
| Epoch (UTC): | 25 May 2026 14:25:31 |
| Eccentricity: | 0.0004605 |
| inclination: | 45.0034° |
| perigee height: | 685 km |
| apogee height: | 691 km |
| right ascension of ascending node: | 56.1266° |
| argument of perigee: | 155.9444° |
| revolutions per day: | 14.61536139 |
| mean anomaly at epoch: | 204.1629° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|