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 23155.44117833 .00000256 00000-0 15810-3 0 9999
2 31793 70.9735 133.3818 0001595 267.7870 264.5067 14.14534318822635
Epoch (UTC): | 04 June 2023 10:35:17 |
Eccentricity: | 0.0001595 |
inclination: | 70.9735° |
perigee height: | 843 km |
apogee height: | 845 km |
right ascension of ascending node: | 133.3818° |
argument of perigee: | 267.7870° |
revolutions per day: | 14.14534318 |
mean anomaly at epoch: | 264.5067° |
orbit number at epoch: | 82263 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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