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 31702U 07027B 23131.88404733 0.00010500 00000-0 12075-2 0 02
2 31702 63.3365 44.6495 0505529 27.4220 332.5780 14.22593914 04
Epoch (UTC): | 11 May 2023 21:13:01 |
Eccentricity: | 0.0505529 |
inclination: | 63.3365° |
perigee height: | 453 km |
apogee height: | 1180 km |
right ascension of ascending node: | 44.6495° |
argument of perigee: | 27.4220° |
revolutions per day: | 14.22593914 |
mean anomaly at epoch: | 332.5780° |
orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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