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 41915U 17002C 24309.29033860 .00069123 00000-0 18036-2 0 9990
2 41915 97.1877 333.5022 0007469 91.2431 268.9671 15.38541918432345
Epoch (UTC): | 04 November 2024 06:58:05 |
Eccentricity: | 0.0007469 |
inclination: | 97.1877° |
perigee height: | 445 km |
apogee height: | 455 km |
right ascension of ascending node: | 333.5022° |
argument of perigee: | 91.2431° |
revolutions per day: | 15.38541918 |
mean anomaly at epoch: | 268.9671° |
orbit number at epoch: | 43234 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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