View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26093U 00004L 23083.58968202 .00006259 00000-0 14887-2 0 9992
2 26093 100.2010 308.1191 0029717 75.2690 285.1790 14.54037724220221
Epoch (UTC): | 24 March 2023 14:09:08 |
Eccentricity: | 0.0029717 |
inclination: | 100.2010° |
perigee height: | 691 km |
apogee height: | 733 km |
right ascension of ascending node: | 308.1191° |
argument of perigee: | 75.2690° |
revolutions per day: | 14.54037724 |
mean anomaly at epoch: | 285.1790° |
orbit number at epoch: | 22022 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|