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 40074U 14037F 23087.21732535 .00008006 00000-0 88957-3 0 9992
2 40074 98.3510 347.4764 0005306 81.4696 278.7227 14.87468669472216
Epoch (UTC): | 28 March 2023 05:12:56 |
Eccentricity: | 0.0005306 |
inclination: | 98.3510° |
perigee height: | 602 km |
apogee height: | 609 km |
right ascension of ascending node: | 347.4764° |
argument of perigee: | 81.4696° |
revolutions per day: | 14.87468669 |
mean anomaly at epoch: | 278.7227° |
orbit number at epoch: | 47221 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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