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 23268.31401902 .00020202 00000-0 12526-2 0 9997
2 18010 63.2944 213.2852 0913036 85.7528 284.7166 13.58789858208657
Epoch (UTC): | 25 September 2023 07:32:11 |
Eccentricity: | 0.0913036 |
inclination: | 63.2944° |
perigee height: | 363 km |
apogee height: | 1717 km |
right ascension of ascending node: | 213.2852° |
argument of perigee: | 85.7528° |
revolutions per day: | 13.58789858 |
mean anomaly at epoch: | 284.7166° |
orbit number at epoch: | 20865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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