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 24284.47111497 .00000245 00000-0 12967-3 0 9999
2 18187 65.0106 309.4357 0020605 264.7452 95.1281 14.31357766946186
Epoch (UTC): | 10 October 2024 11:18:24 |
Eccentricity: | 0.0020605 |
inclination: | 65.0106° |
perigee height: | 772 km |
apogee height: | 802 km |
right ascension of ascending node: | 309.4357° |
argument of perigee: | 264.7452° |
revolutions per day: | 14.31357766 |
mean anomaly at epoch: | 95.1281° |
orbit number at epoch: | 94618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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