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 05175U 71035B 23150.52075890 .00000220 00000-0 80502-4 0 9994
2 05175 74.0465 169.3641 0030269 201.9548 158.0312 14.38358486727078
Epoch (UTC): | 30 May 2023 12:29:53 |
Eccentricity: | 0.0030269 |
inclination: | 74.0465° |
perigee height: | 742 km |
apogee height: | 785 km |
right ascension of ascending node: | 169.3641° |
argument of perigee: | 201.9548° |
revolutions per day: | 14.38358486 |
mean anomaly at epoch: | 158.0312° |
orbit number at epoch: | 72707 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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