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 23157.52663472 .00000277 00000-0 93874-4 0 9998
2 10521 74.0258 190.9504 0020321 28.8751 331.3525 14.41177090386276
Epoch (UTC): | 06 June 2023 12:38:21 |
Eccentricity: | 0.0020321 |
inclination: | 74.0258° |
perigee height: | 740 km |
apogee height: | 769 km |
right ascension of ascending node: | 190.9504° |
argument of perigee: | 28.8751° |
revolutions per day: | 14.41177090 |
mean anomaly at epoch: | 331.3525° |
orbit number at epoch: | 38627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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