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 12658U 81053N 24358.05990924 .00007975 00000-0 34050-2 0 9991
2 12658 82.9709 218.2091 0037796 289.6436 226.3457 14.24540181213232
Epoch (UTC): | 23 December 2024 01:26:16 |
Eccentricity: | 0.0037796 |
inclination: | 82.9709° |
perigee height: | 783 km |
apogee height: | 837 km |
right ascension of ascending node: | 218.2091° |
argument of perigee: | 289.6436° |
revolutions per day: | 14.24540181 |
mean anomaly at epoch: | 226.3457° |
orbit number at epoch: | 21323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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