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 35685U 09041E 24315.51773618 .00007796 00000-0 80375-3 0 9999
2 35685 98.0939 47.5537 0051978 283.2265 76.3157 14.89507559827410
Epoch (UTC): | 10 November 2024 12:25:32 |
Eccentricity: | 0.0051978 |
inclination: | 98.0939° |
perigee height: | 563 km |
apogee height: | 636 km |
right ascension of ascending node: | 47.5537° |
argument of perigee: | 283.2265° |
revolutions per day: | 14.89507559 |
mean anomaly at epoch: | 76.3157° |
orbit number at epoch: | 82741 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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