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 16631U 86014H 23081.27614030 .00014841 00000-0 88320-3 0 9995
2 16631 63.2908 48.4127 0924368 89.0123 281.6542 13.57513282181597
Epoch (UTC): | 22 March 2023 06:37:38 |
Eccentricity: | 0.0924368 |
inclination: | 63.2908° |
perigee height: | 358 km |
apogee height: | 1731 km |
right ascension of ascending node: | 48.4127° |
argument of perigee: | 89.0123° |
revolutions per day: | 13.57513282 |
mean anomaly at epoch: | 281.6542° |
orbit number at epoch: | 18159 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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