View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64351U 26145.33903444 +.00000000 +00000-0 +21487-3 0 00005
2 64351 70.0007 201.1731 0003750 269.0984 90.9746 14.98336272 03
| Epoch (UTC): | 25 May 2026 08:08:12 |
| Eccentricity: | 0.0003750 |
| inclination: | 70.0007° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 201.1731° |
| argument of perigee: | 269.0984° |
| revolutions per day: | 14.98336272 |
| mean anomaly at epoch: | 90.9746° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|