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 40300U 14070C 23083.61696845 .00020201 00000-0 68121-3 0 9996
2 40300 97.1496 132.8466 0015601 238.3627 244.0897 15.30629104465414
Epoch (UTC): | 24 March 2023 14:48:26 |
Eccentricity: | 0.0015601 |
inclination: | 97.1496° |
perigee height: | 463 km |
apogee height: | 484 km |
right ascension of ascending node: | 132.8466° |
argument of perigee: | 238.3627° |
revolutions per day: | 15.30629104 |
mean anomaly at epoch: | 244.0897° |
orbit number at epoch: | 46541 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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