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 46U 60007B 24309.94660449 .00003351 00000-0 64840-3 0 9990
2 46 66.6922 32.7230 0198043 13.5876 347.0455 14.52895888371327
Epoch (UTC): | 04 November 2024 22:43:06 |
Eccentricity: | 0.0198043 |
inclination: | 66.6922° |
perigee height: | 576 km |
apogee height: | 857 km |
right ascension of ascending node: | 32.7230° |
argument of perigee: | 13.5876° |
revolutions per day: | 14.52895888 |
mean anomaly at epoch: | 347.0455° |
orbit number at epoch: | 37132 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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