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 16182U 85097B 23031.34410189 .00000297 00000-0 17388-3 0 9994
2 16182 71.0042 6.0022 0008098 201.0303 308.8286 14.16309366926739
Epoch (UTC): | 31 January 2023 08:15:30 |
Eccentricity: | 0.0008098 |
inclination: | 71.0042° |
perigee height: | 832 km |
apogee height: | 844 km |
right ascension of ascending node: | 6.0022° |
argument of perigee: | 201.0303° |
revolutions per day: | 14.16309366 |
mean anomaly at epoch: | 308.8286° |
orbit number at epoch: | 92673 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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