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 23081.74847557 .01063680 52860-3 27085-2 0 9995
2 40900 97.3551 111.1025 0003814 195.3296 275.7672 15.95502771417681
Epoch (UTC): | 22 March 2023 17:57:48 |
Eccentricity: | 0.0003814 |
inclination: | 97.3551° |
perigee height: | 284 km |
apogee height: | 289 km |
right ascension of ascending node: | 111.1025° |
argument of perigee: | 195.3296° |
revolutions per day: | 15.95502771 |
mean anomaly at epoch: | 275.7672° |
orbit number at epoch: | 41768 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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