View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68503U 26145.61839359 +.00000000 +00000-0 +18458-3 0 00006
2 68503 97.7559 104.1120 0006450 124.6638 235.5189 14.90653589 03
| Epoch (UTC): | 25 May 2026 14:50:29 |
| Eccentricity: | 0.0006450 |
| inclination: | 97.7559° |
| perigee height: | 591 km |
| apogee height: | 600 km |
| right ascension of ascending node: | 104.1120° |
| argument of perigee: | 124.6638° |
| revolutions per day: | 14.90653589 |
| mean anomaly at epoch: | 235.5189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|