View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 22784U 26106.92235993 +.00000000 +00000-0 +27208-4 0 00006
2 22784 82.5529 348.4780 0022817 37.2818 333.1783 13.83547504 07
| Epoch (UTC): | 16 April 2026 22:08:11 |
| Eccentricity: | 0.0022817 |
| inclination: | 82.5529° |
| perigee height: | 935 km |
| apogee height: | 968 km |
| right ascension of ascending node: | 348.4780° |
| argument of perigee: | 37.2818° |
| revolutions per day: | 13.83547504 |
| mean anomaly at epoch: | 333.1783° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|