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 21938U 92020B 23152.16158913 .00000011 00000-0 -42595-5 0 9996
2 21938 82.9305 185.6849 0027888 242.2959 177.9909 13.75353333562246
Epoch (UTC): | 01 June 2023 03:52:41 |
Eccentricity: | 0.0027888 |
inclination: | 82.9305° |
perigee height: | 960 km |
apogee height: | 1001 km |
right ascension of ascending node: | 185.6849° |
argument of perigee: | 242.2959° |
revolutions per day: | 13.75353333 |
mean anomaly at epoch: | 177.9909° |
orbit number at epoch: | 56224 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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