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 40907U 15049J 23334.79898199 .00030448 00000-0 88791-3 0 9999
2 40907 97.4875 344.1955 0006910 291.6933 68.3574 15.35287075453987
Epoch (UTC): | 30 November 2023 19:10:32 |
Eccentricity: | 0.0006910 |
inclination: | 97.4875° |
perigee height: | 455 km |
apogee height: | 465 km |
right ascension of ascending node: | 344.1955° |
argument of perigee: | 291.6933° |
revolutions per day: | 15.35287075 |
mean anomaly at epoch: | 68.3574° |
orbit number at epoch: | 45398 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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