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 13771U 83003B 23147.36095733 .00002708 00000-0 14138-3 0 9993
2 13771 81.1679 19.3386 0043045 1.2153 358.9171 15.14773458201485
Epoch (UTC): | 27 May 2023 08:39:46 |
Eccentricity: | 0.0043045 |
inclination: | 81.1679° |
perigee height: | 492 km |
apogee height: | 551 km |
right ascension of ascending node: | 19.3386° |
argument of perigee: | 1.2153° |
revolutions per day: | 15.14773458 |
mean anomaly at epoch: | 358.9171° |
orbit number at epoch: | 20148 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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