View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 27640U 26066.02191382 +.00000000 +00000-0 +98034-4 0 00006
2 27640 98.7162 74.4553 0014663 143.8235 216.3936 14.19911487 03
| Epoch (UTC): | 07 March 2026 00:31:33 |
| Eccentricity: | 0.0014663 |
| inclination: | 98.7162° |
| perigee height: | 815 km |
| apogee height: | 836 km |
| right ascension of ascending node: | 74.4553° |
| argument of perigee: | 143.8235° |
| revolutions per day: | 14.19911487 |
| mean anomaly at epoch: | 216.3936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|