View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65208U 26145.44681263 +.00000000 +00000-0 +41698-3 0 00007
2 65208 53.1585 155.4024 0001015 78.0577 282.0539 15.34402287 07
| Epoch (UTC): | 25 May 2026 10:43:24 |
| Eccentricity: | 0.0001015 |
| inclination: | 53.1585° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.4024° |
| argument of perigee: | 78.0577° |
| revolutions per day: | 15.34402287 |
| mean anomaly at epoch: | 282.0539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|