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 36597U 10027B 24276.83272566 .00012014 00000-0 99964-3 0 9998
2 36597 98.0517 275.4974 0052715 197.7271 162.2112 14.97747533777538
Epoch (UTC): | 02 October 2024 19:59:07 |
Eccentricity: | 0.0052715 |
inclination: | 98.0517° |
perigee height: | 537 km |
apogee height: | 610 km |
right ascension of ascending node: | 275.4974° |
argument of perigee: | 197.7271° |
revolutions per day: | 14.97747533 |
mean anomaly at epoch: | 162.2112° |
orbit number at epoch: | 77753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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