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 23153.57309140 .00008760 00000-0 30894-3 0 9992
2 12585 97.5757 168.5953 0011395 356.5177 3.5982 15.29449585293398
Epoch (UTC): | 02 June 2023 13:45:15 |
Eccentricity: | 0.0011395 |
inclination: | 97.5757° |
perigee height: | 469 km |
apogee height: | 485 km |
right ascension of ascending node: | 168.5953° |
argument of perigee: | 356.5177° |
revolutions per day: | 15.29449585 |
mean anomaly at epoch: | 3.5982° |
orbit number at epoch: | 29339 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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