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 12673U 81053AD 24358.06860701 .00004992 00000-0 28517-2 0 9995
2 12673 82.8529 212.9951 0042301 6.6433 146.8870 14.08982504198852
Epoch (UTC): | 23 December 2024 01:38:47 |
Eccentricity: | 0.0042301 |
inclination: | 82.8529° |
perigee height: | 832 km |
apogee height: | 893 km |
right ascension of ascending node: | 212.9951° |
argument of perigee: | 6.6433° |
revolutions per day: | 14.08982504 |
mean anomaly at epoch: | 146.8870° |
orbit number at epoch: | 19885 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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