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 23657U 95046A 22144.11497650 .00001359 00000-0 14975-3 0 9990
2 23657 82.5281 7.2878 0020537 232.6122 127.3226 14.86682239445104
Epoch (UTC): | 24 May 2022 02:45:33 |
Eccentricity: | 0.0020537 |
inclination: | 82.5281° |
perigee height: | 594 km |
apogee height: | 622 km |
right ascension of ascending node: | 7.2878° |
argument of perigee: | 232.6122° |
revolutions per day: | 14.86682239 |
mean anomaly at epoch: | 127.3226° |
orbit number at epoch: | 44510 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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