View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64059U 26145.36628138 +.00000000 +00000-0 +53479-4 0 00004
2 64059 44.9785 123.2393 0011959 276.8184 83.1288 13.99146239 04
| Epoch (UTC): | 25 May 2026 08:47:26 |
| Eccentricity: | 0.0011959 |
| inclination: | 44.9785° |
| perigee height: | 888 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 123.2393° |
| argument of perigee: | 276.8184° |
| revolutions per day: | 13.99146239 |
| mean anomaly at epoch: | 83.1288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|