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 19922U 89028B 24311.46527699 .00000278 00000-0 26385-3 0 9993
2 19922 82.9610 224.1509 0035025 243.6147 116.1413 13.77407278788529
Epoch (UTC): | 06 November 2024 11:09:59 |
Eccentricity: | 0.0035025 |
inclination: | 82.9610° |
perigee height: | 947 km |
apogee height: | 999 km |
right ascension of ascending node: | 224.1509° |
argument of perigee: | 243.6147° |
revolutions per day: | 13.77407278 |
mean anomaly at epoch: | 116.1413° |
orbit number at epoch: | 78852 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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