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 15889U 85058A 23336.59739638 .00016017 00000-0 51292-3 0 9991
2 15889 82.4813 164.7001 0013214 101.5223 258.7503 15.32174972100364
Epoch (UTC): | 02 December 2023 14:20:15 |
Eccentricity: | 0.0013214 |
inclination: | 82.4813° |
perigee height: | 460 km |
apogee height: | 478 km |
right ascension of ascending node: | 164.7001° |
argument of perigee: | 101.5223° |
revolutions per day: | 15.32174972 |
mean anomaly at epoch: | 258.7503° |
orbit number at epoch: | 10036 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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