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 37841U 11058D 23147.86535056 .00000441 00000-0 96823-4 0 9994
2 37841 19.9734 332.8921 0011806 168.3147 325.0500 14.10895283600150
Epoch (UTC): | 27 May 2023 20:46:06 |
Eccentricity: | 0.0011806 |
inclination: | 19.9734° |
perigee height: | 848 km |
apogee height: | 865 km |
right ascension of ascending node: | 332.8921° |
argument of perigee: | 168.3147° |
revolutions per day: | 14.10895283 |
mean anomaly at epoch: | 325.0500° |
orbit number at epoch: | 60015 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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