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 18010U 87043F 23080.20585476 .00016317 00000-0 10516-2 0 9995
2 18010 63.2998 356.1907 0931055 82.1437 288.4117 13.54175028183131
Epoch (UTC): | 21 March 2023 04:56:25 |
Eccentricity: | 0.0931055 |
inclination: | 63.2998° |
perigee height: | 364 km |
apogee height: | 1749 km |
right ascension of ascending node: | 356.1907° |
argument of perigee: | 82.1437° |
revolutions per day: | 13.54175028 |
mean anomaly at epoch: | 288.4117° |
orbit number at epoch: | 18313 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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