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 39224U 13035E 22227.50372428 .00000991 00000-0 36657-3 0 9997
2 39224 97.9320 107.3414 0175006 50.1279 311.5147 14.26115331467067
Epoch (UTC): | 15 August 2022 12:05:21 |
Eccentricity: | 0.0175006 |
inclination: | 97.9320° |
perigee height: | 679 km |
apogee height: | 930 km |
right ascension of ascending node: | 107.3414° |
argument of perigee: | 50.1279° |
revolutions per day: | 14.26115331 |
mean anomaly at epoch: | 311.5147° |
orbit number at epoch: | 46706 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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