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 25197.65192348 .00000034 00000-0 41219-4 0 9997
2 16182 71.0027 277.4614 0009681 259.3890 210.7666 14.16554409 53801
Epoch (UTC): | 16 July 2025 15:38:46 |
Eccentricity: | 0.0009681 |
inclination: | 71.0027° |
perigee height: | 830 km |
apogee height: | 844 km |
right ascension of ascending node: | 277.4614° |
argument of perigee: | 259.3890° |
revolutions per day: | 14.16554409 |
mean anomaly at epoch: | 210.7666° |
orbit number at epoch: | 5380 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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