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 43678U 18084H 24261.20125721 .00009217 00000-0 82566-3 0 9993
2 43678 98.0825 61.9826 0010310 87.8580 272.3821 14.96006305320672
Epoch (UTC): | 17 September 2024 04:49:48 |
Eccentricity: | 0.0010310 |
inclination: | 98.0825° |
perigee height: | 572 km |
apogee height: | 586 km |
right ascension of ascending node: | 61.9826° |
argument of perigee: | 87.8580° |
revolutions per day: | 14.96006305 |
mean anomaly at epoch: | 272.3821° |
orbit number at epoch: | 32067 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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