View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 07530U 74089B 22180.55986262 -.00000050 00000-0 -24003-4 0 9999
2 07530 101.9043 160.4681 0012465 20.6043 88.4972 12.53655573178987
Epoch (UTC): | 29 June 2022 13:26:12 |
Eccentricity: | 0.0012465 |
inclination: | 101.9043° |
perigee height: | 1439 km |
apogee height: | 1459 km |
right ascension of ascending node: | 160.4681° |
argument of perigee: | 20.6043° |
revolutions per day: | 12.53655573 |
mean anomaly at epoch: | 88.4972° |
orbit number at epoch: | 17898 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|