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 39417U 13066B 22179.50503966 .00001285 00000-0 16240-3 0 9997
2 39417 97.6367 150.5028 0058135 10.1180 350.1189 14.82379832464769
Epoch (UTC): | 28 June 2022 12:07:15 |
Eccentricity: | 0.0058135 |
inclination: | 97.6367° |
perigee height: | 581 km |
apogee height: | 662 km |
right ascension of ascending node: | 150.5028° |
argument of perigee: | 10.1180° |
revolutions per day: | 14.82379832 |
mean anomaly at epoch: | 350.1189° |
orbit number at epoch: | 46476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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