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 16494U 86005B 25188.57480310 .00000029 00000-0 14074-4 0 9996
2 16494 82.9307 43.0297 0018181 291.3199 128.1571 13.76747952982468
Epoch (UTC): | 07 July 2025 13:47:42 |
Eccentricity: | 0.0018181 |
inclination: | 82.9307° |
perigee height: | 962 km |
apogee height: | 989 km |
right ascension of ascending node: | 43.0297° |
argument of perigee: | 291.3199° |
revolutions per day: | 13.76747952 |
mean anomaly at epoch: | 128.1571° |
orbit number at epoch: | 98246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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