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 15483U 85006B 25199.80429269 .00000170 00000-0 65177-4 0 9994
2 15483 74.0473 331.4420 0019261 302.6999 209.6207 14.37610776120418
Epoch (UTC): | 18 July 2025 19:18:10 |
Eccentricity: | 0.0019261 |
inclination: | 74.0473° |
perigee height: | 752 km |
apogee height: | 780 km |
right ascension of ascending node: | 331.4420° |
argument of perigee: | 302.6999° |
revolutions per day: | 14.37610776 |
mean anomaly at epoch: | 209.6207° |
orbit number at epoch: | 12041 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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