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 51U 60009C 23087.98848852 -.00000052 00000-0 31003-3 0 9991
2 51 47.2122 88.6801 0109579 298.8468 60.1358 12.18297401787766
Epoch (UTC): | 28 March 2023 23:43:25 |
Eccentricity: | 0.0109579 |
inclination: | 47.2122° |
perigee height: | 1512 km |
apogee height: | 1687 km |
right ascension of ascending node: | 88.6801° |
argument of perigee: | 298.8468° |
revolutions per day: | 12.18297401 |
mean anomaly at epoch: | 60.1358° |
orbit number at epoch: | 78776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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