View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68166U 26145.58335647 +.00000000 +00000-0 +74572-4 0 00008
2 68166 97.2851 168.0686 0001647 90.8774 0.2715 15.33446438 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001647 |
| inclination: | 97.2851° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 168.0686° |
| argument of perigee: | 90.8774° |
| revolutions per day: | 15.33446438 |
| mean anomaly at epoch: | 0.2715° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|