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 17911U 87038A 23161.40993421 .00005080 00000-0 24678-3 0 9993
2 17911 82.5207 212.6221 0007909 263.3059 96.7275 15.18214001971729
Epoch (UTC): | 10 June 2023 09:50:18 |
Eccentricity: | 0.0007909 |
inclination: | 82.5207° |
perigee height: | 506 km |
apogee height: | 516 km |
right ascension of ascending node: | 212.6221° |
argument of perigee: | 263.3059° |
revolutions per day: | 15.18214001 |
mean anomaly at epoch: | 96.7275° |
orbit number at epoch: | 97172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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