View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68433U 26145.63780791 +.00000000 +00000-0 +25338-3 0 00000
2 68433 97.4554 104.3637 0007135 127.3242 232.8642 15.17141138 00
| Epoch (UTC): | 25 May 2026 15:18:26 |
| Eccentricity: | 0.0007135 |
| inclination: | 97.4554° |
| perigee height: | 510 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 104.3637° |
| argument of perigee: | 127.3242° |
| revolutions per day: | 15.17141138 |
| mean anomaly at epoch: | 232.8642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|