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 24261.14066773 .00276043 00000-0 25674-2 0 9996
2 40907 97.4630 284.7208 0001032 313.7182 46.3993 15.66531252499005
Epoch (UTC): | 17 September 2024 03:22:33 |
Eccentricity: | 0.0001032 |
inclination: | 97.4630° |
perigee height: | 368 km |
apogee height: | 369 km |
right ascension of ascending node: | 284.7208° |
argument of perigee: | 313.7182° |
revolutions per day: | 15.66531252 |
mean anomaly at epoch: | 46.3993° |
orbit number at epoch: | 49900 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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