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 23148.46496608 .00011341 00000-0 41916-3 0 9994
2 40907 97.4922 156.0240 0009688 214.1063 145.9555 15.27845598425471
Epoch (UTC): | 28 May 2023 11:09:33 |
Eccentricity: | 0.0009688 |
inclination: | 97.4922° |
perigee height: | 475 km |
apogee height: | 489 km |
right ascension of ascending node: | 156.0240° |
argument of perigee: | 214.1063° |
revolutions per day: | 15.27845598 |
mean anomaly at epoch: | 145.9555° |
orbit number at epoch: | 42547 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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