View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68626U 26145.09090832 +.00000000 +00000-0 +13337-2 0 00009
2 68626 97.2852 344.6285 0001480 81.5547 278.5886 15.75187692 03
| Epoch (UTC): | 25 May 2026 02:10:54 |
| Eccentricity: | 0.0001480 |
| inclination: | 97.2852° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 344.6285° |
| argument of perigee: | 81.5547° |
| revolutions per day: | 15.75187692 |
| mean anomaly at epoch: | 278.5886° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|