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 40900U 15049B 23086.17456750 .02657980 12271-1 29717-2 0 9995
2 40900 97.3362 116.0138 0002935 288.0689 145.3019 16.12602764418398
Epoch (UTC): | 27 March 2023 04:11:22 |
Eccentricity: | 0.0002935 |
inclination: | 97.3362° |
perigee height: | 238 km |
apogee height: | 241 km |
right ascension of ascending node: | 116.0138° |
argument of perigee: | 288.0689° |
revolutions per day: | 16.12602764 |
mean anomaly at epoch: | 145.3019° |
orbit number at epoch: | 41839 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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