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 25560U 98071A 25137.21615745 .00003337 00000-0 23566-3 0 9993
2 25560 69.8951 165.7051 0005356 178.5363 181.5816 15.05933309437849
Epoch (UTC): | 17 May 2025 05:11:16 |
Eccentricity: | 0.0005356 |
inclination: | 69.8951° |
perigee height: | 545 km |
apogee height: | 552 km |
right ascension of ascending node: | 165.7051° |
argument of perigee: | 178.5363° |
revolutions per day: | 15.05933309 |
mean anomaly at epoch: | 181.5816° |
orbit number at epoch: | 43784 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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