View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28654U 05018A 23332.13437329 .00000401 00000-0 23836-3 0 9994
2 28654 98.8962 45.6230 0013287 275.8607 84.1050 14.13065000954720
Epoch (UTC): | 28 November 2023 03:13:29 |
Eccentricity: | 0.0013287 |
inclination: | 98.8962° |
perigee height: | 839 km |
apogee height: | 858 km |
right ascension of ascending node: | 45.6230° |
argument of perigee: | 275.8607° |
revolutions per day: | 14.13065000 |
mean anomaly at epoch: | 84.1050° |
orbit number at epoch: | 95472 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|