View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 00670U 26053.70558969 +.00000000 +00000-0 +16838-3 0 00000
2 00670 89.9743 333.2925 0041872 4.9001 355.2548 13.44664917 05
| Epoch (UTC): | 22 February 2026 16:56:02 |
| Eccentricity: | 0.0041872 |
| inclination: | 89.9743° |
| perigee height: | 1061 km |
| apogee height: | 1123 km |
| right ascension of ascending node: | 333.2925° |
| argument of perigee: | 4.9001° |
| revolutions per day: | 13.44664917 |
| mean anomaly at epoch: | 355.2548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|