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 40071U 14037C 23337.77864758 .00003244 00000-0 39877-3 0 9997
2 40071 98.3425 236.4123 0009110 44.7352 315.4594 14.83752198508509
Epoch (UTC): | 03 December 2023 18:41:15 |
Eccentricity: | 0.0009110 |
inclination: | 98.3425° |
perigee height: | 611 km |
apogee height: | 624 km |
right ascension of ascending node: | 236.4123° |
argument of perigee: | 44.7352° |
revolutions per day: | 14.83752198 |
mean anomaly at epoch: | 315.4594° |
orbit number at epoch: | 50850 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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