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 23090.71525951 .00007492 00000-0 83185-3 0 9999
2 40074 98.3493 351.1568 0005263 66.9739 293.2007 14.87518584472735
Epoch (UTC): | 31 March 2023 17:09:58 |
Eccentricity: | 0.0005263 |
inclination: | 98.3493° |
perigee height: | 602 km |
apogee height: | 609 km |
right ascension of ascending node: | 351.1568° |
argument of perigee: | 66.9739° |
revolutions per day: | 14.87518584 |
mean anomaly at epoch: | 293.2007° |
orbit number at epoch: | 47273 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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