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 12585U 81065A 23156.58259025 .00008038 00000-0 28335-3 0 9997
2 12585 97.5751 171.6620 0011039 345.3100 14.7818 15.29496576288034
Epoch (UTC): | 05 June 2023 13:58:55 |
Eccentricity: | 0.0011039 |
inclination: | 97.5751° |
perigee height: | 470 km |
apogee height: | 485 km |
right ascension of ascending node: | 171.6620° |
argument of perigee: | 345.3100° |
revolutions per day: | 15.29496576 |
mean anomaly at epoch: | 14.7818° |
orbit number at epoch: | 28803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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