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 24314.11587431 .01165477 75545-3 18405-2 0 9993
2 40907 97.4411 341.9299 0003196 145.3124 214.8365 16.04037535507368
Epoch (UTC): | 09 November 2024 02:46:51 |
Eccentricity: | 0.0003196 |
inclination: | 97.4411° |
perigee height: | 261 km |
apogee height: | 265 km |
right ascension of ascending node: | 341.9299° |
argument of perigee: | 145.3124° |
revolutions per day: | 16.04037535 |
mean anomaly at epoch: | 214.8365° |
orbit number at epoch: | 50736 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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