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 31001U 99025BCT 24277.97504800 .00007240 00000-0 20070-2 0 9999
2 31001 99.3166 106.2405 0152131 348.3841 11.3849 14.40291441919480
Epoch (UTC): | 03 October 2024 23:24:04 |
Eccentricity: | 0.0152131 |
inclination: | 99.3166° |
perigee height: | 649 km |
apogee height: | 866 km |
right ascension of ascending node: | 106.2405° |
argument of perigee: | 348.3841° |
revolutions per day: | 14.40291441 |
mean anomaly at epoch: | 11.3849° |
orbit number at epoch: | 91948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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