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 25860U 99039A 24260.09974291 .00002690 00000-0 37270-3 0 9995
2 25860 98.0271 312.2934 0000869 86.5628 273.5682 14.78833721354685
Epoch (UTC): | 16 September 2024 02:23:37 |
Eccentricity: | 0.0000869 |
inclination: | 98.0271° |
perigee height: | 632 km |
apogee height: | 633 km |
right ascension of ascending node: | 312.2934° |
argument of perigee: | 86.5628° |
revolutions per day: | 14.78833721 |
mean anomaly at epoch: | 273.5682° |
orbit number at epoch: | 35468 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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