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 43131U 18004W 23081.77847083 .00628070 00000-0 26067-2 0 9999
2 43131 97.3318 170.9658 0004983 279.7429 80.3278 15.84212253289623
Epoch (UTC): | 22 March 2023 18:40:59 |
Eccentricity: | 0.0004983 |
inclination: | 97.3318° |
perigee height: | 315 km |
apogee height: | 322 km |
right ascension of ascending node: | 170.9658° |
argument of perigee: | 279.7429° |
revolutions per day: | 15.84212253 |
mean anomaly at epoch: | 80.3278° |
orbit number at epoch: | 28962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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