View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68807U 26145.56330140 +.00000000 +00000-0 +15304-2 0 00007
2 68807 97.2833 352.2217 0001447 92.5583 267.5848 15.75266858 06
| Epoch (UTC): | 25 May 2026 13:31:09 |
| Eccentricity: | 0.0001447 |
| inclination: | 97.2833° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 352.2217° |
| argument of perigee: | 92.5583° |
| revolutions per day: | 15.75266858 |
| mean anomaly at epoch: | 267.5848° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|