View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68468U 26145.37541914 +.00000000 +00000-0 +44278-3 0 00005
2 68468 97.4535 104.0916 0008432 125.2579 234.9444 15.17269979 02
| Epoch (UTC): | 25 May 2026 09:00:36 |
| Eccentricity: | 0.0008432 |
| inclination: | 97.4535° |
| perigee height: | 508 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 104.0916° |
| argument of perigee: | 125.2579° |
| revolutions per day: | 15.17269979 |
| mean anomaly at epoch: | 234.9444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|