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 40028U 14033U 23083.61608643 .00009962 00000-0 97471-3 0 9992
2 40028 98.0015 30.4110 0011168 208.0948 151.9702 14.92479624475971
Epoch (UTC): | 24 March 2023 14:47:09 |
Eccentricity: | 0.0011168 |
inclination: | 98.0015° |
perigee height: | 582 km |
apogee height: | 598 km |
right ascension of ascending node: | 30.4110° |
argument of perigee: | 208.0948° |
revolutions per day: | 14.92479624 |
mean anomaly at epoch: | 151.9702° |
orbit number at epoch: | 47597 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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