View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 29092U 06015A 23150.05140200 .00000826 00000-0 10522-3 0 9996
2 29092 97.8392 177.5884 0001529 92.6359 267.5030 14.84132607924434
Epoch (UTC): | 30 May 2023 01:14:01 |
Eccentricity: | 0.0001529 |
inclination: | 97.8392° |
perigee height: | 615 km |
apogee height: | 617 km |
right ascension of ascending node: | 177.5884° |
argument of perigee: | 92.6359° |
revolutions per day: | 14.84132607 |
mean anomaly at epoch: | 267.5030° |
orbit number at epoch: | 92443 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|