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 16791U 86046A 25196.90849660 .00004064 00000-0 17782-3 0 9995
2 16791 82.4613 21.4634 0017183 83.1117 277.2072 15.21642786130015
Epoch (UTC): | 15 July 2025 21:48:14 |
Eccentricity: | 0.0017183 |
inclination: | 82.4613° |
perigee height: | 489 km |
apogee height: | 513 km |
right ascension of ascending node: | 21.4634° |
argument of perigee: | 83.1117° |
revolutions per day: | 15.21642786 |
mean anomaly at epoch: | 277.2072° |
orbit number at epoch: | 13001 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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