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 40677U 95015FR 23322.78448004 .00000525 00000-0 23484-3 0 9997
2 40677 98.6375 337.6755 0050616 136.2887 224.2318 14.26068744446135
Epoch (UTC): | 18 November 2023 18:49:39 |
Eccentricity: | 0.0050616 |
inclination: | 98.6375° |
perigee height: | 768 km |
apogee height: | 841 km |
right ascension of ascending node: | 337.6755° |
argument of perigee: | 136.2887° |
revolutions per day: | 14.26068744 |
mean anomaly at epoch: | 224.2318° |
orbit number at epoch: | 44613 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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