View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 00029U 60002B 22176.38262890 .00000183 00000-0 57922-4 0 9996
2 00029 48.3806 65.5786 0023703 150.8207 209.4034 14.74661788327430
Epoch (UTC): | 25 June 2022 09:10:59 |
Eccentricity: | 0.0023703 |
inclination: | 48.3806° |
perigee height: | 629 km |
apogee height: | 663 km |
right ascension of ascending node: | 65.5786° |
argument of perigee: | 150.8207° |
revolutions per day: | 14.74661788 |
mean anomaly at epoch: | 209.4034° |
orbit number at epoch: | 32743 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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