View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 68619U 26145.58335647 +.00000000 +00000-0 -26323-1 0 00000
2 68619 97.2845 345.1315 0001853 85.2480 146.3698 15.60251212 05
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001853 |
| inclination: | 97.2845° |
| perigee height: | 386 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 345.1315° |
| argument of perigee: | 85.2480° |
| revolutions per day: | 15.60251212 |
| mean anomaly at epoch: | 146.3698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|