View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68298U 26145.34489778 +.00000000 +00000-0 +10737-2 0 00004
2 68298 97.2851 271.6199 0001275 81.2055 278.9355 15.75216099 02
| Epoch (UTC): | 25 May 2026 08:16:39 |
| Eccentricity: | 0.0001275 |
| inclination: | 97.2851° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6199° |
| argument of perigee: | 81.2055° |
| revolutions per day: | 15.75216099 |
| mean anomaly at epoch: | 278.9355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|