View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 18313U 26108.90255742 +.00000000 +00000-0 +31148-4 0 00001
2 18313 82.5601 348.9559 0008869 236.1037 123.9281 13.84305041 01
| Epoch (UTC): | 18 April 2026 21:39:40 |
| Eccentricity: | 0.0008869 |
| inclination: | 82.5601° |
| perigee height: | 942 km |
| apogee height: | 955 km |
| right ascension of ascending node: | 348.9559° |
| argument of perigee: | 236.1037° |
| revolutions per day: | 13.84305041 |
| mean anomaly at epoch: | 123.9281° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|