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 14506U 83113A 23159.46849531 .00000307 00000-0 13884-3 0 9999
2 14506 98.2980 334.4560 0009863 253.1843 160.8948 14.28520535 57699
Epoch (UTC): | 08 June 2023 11:14:37 |
Eccentricity: | 0.0009863 |
inclination: | 98.2980° |
perigee height: | 789 km |
apogee height: | 804 km |
right ascension of ascending node: | 334.4560° |
argument of perigee: | 253.1843° |
revolutions per day: | 14.28520535 |
mean anomaly at epoch: | 160.8948° |
orbit number at epoch: | 5769 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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