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 42787U 17036Y 23082.85965328 .00153169 00000-0 18484-2 0 9998
2 42787 97.1567 129.4737 0003228 70.7100 289.4642 15.60238871320144
Epoch (UTC): | 23 March 2023 20:37:54 |
Eccentricity: | 0.0003228 |
inclination: | 97.1567° |
perigee height: | 385 km |
apogee height: | 389 km |
right ascension of ascending node: | 129.4737° |
argument of perigee: | 70.7100° |
revolutions per day: | 15.60238871 |
mean anomaly at epoch: | 289.4642° |
orbit number at epoch: | 32014 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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