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 15755U 85042A 23032.30388922 -.00000038 00000-0 40912-5 0 9990
2 15755 71.1134 353.1330 0032992 99.5784 260.9073 14.20538169952256
Epoch (UTC): | 01 February 2023 07:17:36 |
Eccentricity: | 0.0032992 |
inclination: | 71.1134° |
perigee height: | 800 km |
apogee height: | 847 km |
right ascension of ascending node: | 353.1330° |
argument of perigee: | 99.5784° |
revolutions per day: | 14.20538169 |
mean anomaly at epoch: | 260.9073° |
orbit number at epoch: | 95225 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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