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 10521U 77119B 23156.55481548 .00000273 00000-0 92599-4 0 9991
2 10521 74.0259 192.7504 0020288 30.9838 329.2509 14.41176409385820
Epoch (UTC): | 05 June 2023 13:18:56 |
Eccentricity: | 0.0020288 |
inclination: | 74.0259° |
perigee height: | 740 km |
apogee height: | 769 km |
right ascension of ascending node: | 192.7504° |
argument of perigee: | 30.9838° |
revolutions per day: | 14.41176409 |
mean anomaly at epoch: | 329.2509° |
orbit number at epoch: | 38582 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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