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 45510U 79095CS 24251.41600478 .00009761 00000-0 48478-2 0 9995
2 45510 81.1913 128.3135 0018055 292.1757 67.7501 14.16933746350485
Epoch (UTC): | 07 September 2024 09:59:02 |
Eccentricity: | 0.0018055 |
inclination: | 81.1913° |
perigee height: | 823 km |
apogee height: | 849 km |
right ascension of ascending node: | 128.3135° |
argument of perigee: | 292.1757° |
revolutions per day: | 14.16933746 |
mean anomaly at epoch: | 67.7501° |
orbit number at epoch: | 35048 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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