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 44339U 19036A 22181.22101332 .00001557 00000-0 30518-3 0 9998
2 44339 24.0001 112.8734 0010202 358.1270 1.9183 14.55113807160216
Epoch (UTC): | 30 June 2022 05:18:15 |
Eccentricity: | 0.0010202 |
inclination: | 24.0001° |
perigee height: | 702 km |
apogee height: | 716 km |
right ascension of ascending node: | 112.8734° |
argument of perigee: | 358.1270° |
revolutions per day: | 14.55113807 |
mean anomaly at epoch: | 1.9183° |
orbit number at epoch: | 16021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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