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 746U 64006A 22229.16198778 .00001018 00000-0 30698-3 0 9996
2 746 60.8560 276.3946 3021176 229.3866 100.2550 9.04595212940156
Epoch (UTC): | 17 August 2022 03:53:15 |
Eccentricity: | 0.3021176 |
inclination: | 60.8560° |
perigee height: | 412 km |
apogee height: | 6291 km |
right ascension of ascending node: | 276.3946° |
argument of perigee: | 229.3866° |
revolutions per day: | 9.04595212 |
mean anomaly at epoch: | 100.2550° |
orbit number at epoch: | 94015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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