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 20437U 90005B 23080.92613738 .00000235 00000-0 10395-3 0 9993
2 20437 98.9085 85.9074 0011457 125.7250 294.3971 14.32552226732133
Epoch (UTC): | 21 March 2023 22:13:38 |
Eccentricity: | 0.0011457 |
inclination: | 98.9085° |
perigee height: | 775 km |
apogee height: | 791 km |
right ascension of ascending node: | 85.9074° |
argument of perigee: | 125.7250° |
revolutions per day: | 14.32552226 |
mean anomaly at epoch: | 294.3971° |
orbit number at epoch: | 73213 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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