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 13066U 82012B 24281.56644394 .00000298 00000-0 28349-3 0 9995
2 13066 82.9014 22.7150 0042806 329.8147 40.3775 13.77305594142381
Epoch (UTC): | 07 October 2024 13:35:40 |
Eccentricity: | 0.0042806 |
inclination: | 82.9014° |
perigee height: | 942 km |
apogee height: | 1005 km |
right ascension of ascending node: | 22.7150° |
argument of perigee: | 329.8147° |
revolutions per day: | 13.77305594 |
mean anomaly at epoch: | 40.3775° |
orbit number at epoch: | 14238 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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