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 00046U 60007B 24306.64237416 .00002972 00000-0 57835-3 0 9992
2 00046 66.6925 41.7017 0197801 16.0830 344.6436 14.52869582370853
Epoch (UTC): | 01 November 2024 15:25:01 |
Eccentricity: | 0.0197801 |
inclination: | 66.6925° |
perigee height: | 576 km |
apogee height: | 856 km |
right ascension of ascending node: | 41.7017° |
argument of perigee: | 16.0830° |
revolutions per day: | 14.52869582 |
mean anomaly at epoch: | 344.6436° |
orbit number at epoch: | 37085 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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