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 40906U 15049H 24260.17191816 .00065966 00000-0 11030-2 0 9995
2 40906 97.4730 279.8433 0004624 353.5880 6.5312 15.51675159498536
Epoch (UTC): | 16 September 2024 04:07:33 |
Eccentricity: | 0.0004624 |
inclination: | 97.4730° |
perigee height: | 409 km |
apogee height: | 415 km |
right ascension of ascending node: | 279.8433° |
argument of perigee: | 353.5880° |
revolutions per day: | 15.51675159 |
mean anomaly at epoch: | 6.5312° |
orbit number at epoch: | 49853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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