View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68618U 26145.58335647 +.00000000 +00000-0 -31261-3 0 00008
2 68618 97.2847 345.0261 0001799 83.3359 267.1226 15.49220977 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001799 |
| inclination: | 97.2847° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 345.0261° |
| argument of perigee: | 83.3359° |
| revolutions per day: | 15.49220977 |
| mean anomaly at epoch: | 267.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|