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 00047U 60007C 24313.89805782 .00002030 00000-0 45700-3 0 9998
2 00047 66.6650 178.4181 0226084 209.3942 149.4294 14.44079804366259
Epoch (UTC): | 08 November 2024 21:33:12 |
Eccentricity: | 0.0226084 |
inclination: | 66.6650° |
perigee height: | 584 km |
apogee height: | 906 km |
right ascension of ascending node: | 178.4181° |
argument of perigee: | 209.3942° |
revolutions per day: | 14.44079804 |
mean anomaly at epoch: | 149.4294° |
orbit number at epoch: | 36625 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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