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 24312.49357810 .00003091 00000-0 59918-3 0 9990
2 46 66.6919 25.8017 0198275 11.6682 348.8922 14.52913293371699
Epoch (UTC): | 07 November 2024 11:50:45 |
Eccentricity: | 0.0198275 |
inclination: | 66.6919° |
perigee height: | 575 km |
apogee height: | 857 km |
right ascension of ascending node: | 25.8017° |
argument of perigee: | 11.6682° |
revolutions per day: | 14.52913293 |
mean anomaly at epoch: | 348.8922° |
orbit number at epoch: | 37169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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