View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39430U 13066Q 23092.19996190 .00002930 00000-0 51775-3 0 9997
2 39430 97.7885 347.7564 0145417 213.3065 145.8927 14.61443486498449
Epoch (UTC): | 02 April 2023 04:47:56 |
Eccentricity: | 0.0145417 |
inclination: | 97.7885° |
perigee height: | 586 km |
apogee height: | 791 km |
right ascension of ascending node: | 347.7564° |
argument of perigee: | 213.3065° |
revolutions per day: | 14.61443486 |
mean anomaly at epoch: | 145.8927° |
orbit number at epoch: | 49844 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|