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 42761U 17034D 25136.34529264 .00060126 00000-0 68022-3 0 9993
2 42761 43.0108 103.3926 0019356 129.0398 231.2193 15.61357803438823
Epoch (UTC): | 16 May 2025 08:17:13 |
Eccentricity: | 0.0019356 |
inclination: | 43.0108° |
perigee height: | 370 km |
apogee height: | 397 km |
right ascension of ascending node: | 103.3926° |
argument of perigee: | 129.0398° |
revolutions per day: | 15.61357803 |
mean anomaly at epoch: | 231.2193° |
orbit number at epoch: | 43882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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