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 13553U 82092B 25200.53712035 .00000389 00000-0 41274-4 0 9995
2 13553 82.5686 359.4398 0020421 359.0086 68.1341 14.86344893315377
Epoch (UTC): | 19 July 2025 12:53:27 |
Eccentricity: | 0.0020421 |
inclination: | 82.5686° |
perigee height: | 595 km |
apogee height: | 623 km |
right ascension of ascending node: | 359.4398° |
argument of perigee: | 359.0086° |
revolutions per day: | 14.86344893 |
mean anomaly at epoch: | 68.1341° |
orbit number at epoch: | 31537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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