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 23753U 95072C 23151.57882394 .00000040 00000-0 35250-4 0 9994
2 23753 98.8538 202.6725 0004745 87.9263 272.2460 14.26672530427251
Epoch (UTC): | 31 May 2023 13:53:30 |
Eccentricity: | 0.0004745 |
inclination: | 98.8538° |
perigee height: | 799 km |
apogee height: | 806 km |
right ascension of ascending node: | 202.6725° |
argument of perigee: | 87.9263° |
revolutions per day: | 14.26672530 |
mean anomaly at epoch: | 272.2460° |
orbit number at epoch: | 42725 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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