View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56166U 26145.61104701 +.00000000 +00000-0 +66889-4 0 00006
2 56166 80.9996 92.8996 0013299 12.5699 347.5787 13.86945811 03
| Epoch (UTC): | 25 May 2026 14:39:54 |
| Eccentricity: | 0.0013299 |
| inclination: | 80.9996° |
| perigee height: | 930 km |
| apogee height: | 949 km |
| right ascension of ascending node: | 92.8996° |
| argument of perigee: | 12.5699° |
| revolutions per day: | 13.86945811 |
| mean anomaly at epoch: | 347.5787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|