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 18187U 87060A 24310.53197629 .00000276 00000-0 14130-3 0 9995
2 18187 65.0106 236.4648 0020325 263.3528 96.5243 14.31375141949910
Epoch (UTC): | 05 November 2024 12:46:02 |
Eccentricity: | 0.0020325 |
inclination: | 65.0106° |
perigee height: | 772 km |
apogee height: | 802 km |
right ascension of ascending node: | 236.4648° |
argument of perigee: | 263.3528° |
revolutions per day: | 14.31375141 |
mean anomaly at epoch: | 96.5243° |
orbit number at epoch: | 94991 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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