View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00029U 60002B 22219.40813307 .00000056 00000-0 39027-4 0 9997
2 00029 48.3780 222.4273 0024340 332.7700 27.1935 14.74692786333785
Epoch (UTC): | 07 August 2022 09:47:42 |
Eccentricity: | 0.0024340 |
inclination: | 48.3780° |
perigee height: | 629 km |
apogee height: | 663 km |
right ascension of ascending node: | 222.4273° |
argument of perigee: | 332.7700° |
revolutions per day: | 14.74692786 |
mean anomaly at epoch: | 27.1935° |
orbit number at epoch: | 33378 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|