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 23341.75743047 .00001676 00000-0 20947-3 0 9992
2 40071 98.3431 240.5692 0008898 33.0373 327.1394 14.83766090509098
Epoch (UTC): | 07 December 2023 18:10:41 |
Eccentricity: | 0.0008898 |
inclination: | 98.3431° |
perigee height: | 611 km |
apogee height: | 623 km |
right ascension of ascending node: | 240.5692° |
argument of perigee: | 33.0373° |
revolutions per day: | 14.83766090 |
mean anomaly at epoch: | 327.1394° |
orbit number at epoch: | 50909 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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