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 40016U 14033G 23083.47069809 .00001713 00000-0 25165-3 0 9995
2 40016 97.6393 267.9151 0046718 313.8935 45.8421 14.75998417471695
Epoch (UTC): | 24 March 2023 11:17:48 |
Eccentricity: | 0.0046718 |
inclination: | 97.6393° |
perigee height: | 609 km |
apogee height: | 675 km |
right ascension of ascending node: | 267.9151° |
argument of perigee: | 313.8935° |
revolutions per day: | 14.75998417 |
mean anomaly at epoch: | 45.8421° |
orbit number at epoch: | 47169 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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