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 25544U 98067A 23276.14841953 .00021513 00000-0 38752-3 0 9995
2 25544 51.6417 153.7837 0005276 66.6793 83.0521 15.49723616418531
Epoch (UTC): | 03 October 2023 03:33:43 |
Eccentricity: | 0.0005276 |
inclination: | 51.6417° |
perigee height: | 414 km |
apogee height: | 421 km |
right ascension of ascending node: | 153.7837° |
argument of perigee: | 66.6793° |
revolutions per day: | 15.49723616 |
mean anomaly at epoch: | 83.0521° |
orbit number at epoch: | 41853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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