View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65191U 26145.58886670 +.00000000 +00000-0 +21349-3 0 00003
2 65191 97.4520 18.0984 0002113 81.3326 278.8141 15.05656276 05
| Epoch (UTC): | 25 May 2026 14:07:58 |
| Eccentricity: | 0.0002113 |
| inclination: | 97.4520° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 18.0984° |
| argument of perigee: | 81.3326° |
| revolutions per day: | 15.05656276 |
| mean anomaly at epoch: | 278.8141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|