View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68647U 26144.42294242 +.00000000 +00000-0 +37990-4 0 00002
2 68647 88.9864 323.4377 0010882 80.3697 279.8692 13.66001667 06
| Epoch (UTC): | 24 May 2026 10:09:02 |
| Eccentricity: | 0.0010882 |
| inclination: | 88.9864° |
| perigee height: | 1006 km |
| apogee height: | 1022 km |
| right ascension of ascending node: | 323.4377° |
| argument of perigee: | 80.3697° |
| revolutions per day: | 13.66001667 |
| mean anomaly at epoch: | 279.8692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|