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 41879U 16075A 23266.52723021 -.00000206 00000-0 00000-0 0 9998
2 41879 0.0131 102.8742 0000252 78.0007 160.8350 1.00270615 24811
Epoch (UTC): | 23 September 2023 12:39:12 |
Eccentricity: | 0.0000252 |
inclination: | 0.0131° |
perigee height: | 35785 km |
apogee height: | 35787 km |
right ascension of ascending node: | 102.8742° |
argument of perigee: | 78.0007° |
revolutions per day: | 1.00270615 |
mean anomaly at epoch: | 160.8350° |
orbit number at epoch: | 2481 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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