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 43144U 18004AK 23096.66823740 .07616265 24404-5 15827-2 0 9992
2 43144 97.3132 188.9946 0013310 281.8266 78.1536 16.30823601292079
Epoch (UTC): | 06 April 2023 16:02:15 |
Eccentricity: | 0.0013310 |
inclination: | 97.3132° |
perigee height: | 181 km |
apogee height: | 199 km |
right ascension of ascending node: | 188.9946° |
argument of perigee: | 281.8266° |
revolutions per day: | 16.30823601 |
mean anomaly at epoch: | 78.1536° |
orbit number at epoch: | 29207 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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