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 19257U 88053B 23160.50490253 .00000326 00000-0 11653-3 0 9998
2 19257 74.0460 161.7992 0021424 233.8560 243.4781 14.37847134832219
Epoch (UTC): | 09 June 2023 12:07:03 |
Eccentricity: | 0.0021424 |
inclination: | 74.0460° |
perigee height: | 750 km |
apogee height: | 781 km |
right ascension of ascending node: | 161.7992° |
argument of perigee: | 233.8560° |
revolutions per day: | 14.37847134 |
mean anomaly at epoch: | 243.4781° |
orbit number at epoch: | 83221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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