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 31793U 07029B 23149.71334177 .00000082 00000-0 67719-4 0 9997
2 31793 70.9726 145.4166 0001670 264.4866 268.5186 14.14531592821825
Epoch (UTC): | 29 May 2023 17:07:12 |
Eccentricity: | 0.0001670 |
inclination: | 70.9726° |
perigee height: | 843 km |
apogee height: | 845 km |
right ascension of ascending node: | 145.4166° |
argument of perigee: | 264.4866° |
revolutions per day: | 14.14531592 |
mean anomaly at epoch: | 268.5186° |
orbit number at epoch: | 82182 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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