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 18123U 87053A 23081.77857840 .00000358 00000-0 19241-3 0 9994
2 18123 98.7261 269.1902 0011909 324.6326 35.4059 14.18989956849349
Epoch (UTC): | 22 March 2023 18:41:09 |
Eccentricity: | 0.0011909 |
inclination: | 98.7261° |
perigee height: | 820 km |
apogee height: | 837 km |
right ascension of ascending node: | 269.1902° |
argument of perigee: | 324.6326° |
revolutions per day: | 14.18989956 |
mean anomaly at epoch: | 35.4059° |
orbit number at epoch: | 84934 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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