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 23268.27860045 .00019455 00000-0 35229-3 0 9991
2 25544 51.6420 192.7535 0005874 59.8797 75.3053 15.49641125417318
Epoch (UTC): | 25 September 2023 06:41:11 |
Eccentricity: | 0.0005874 |
inclination: | 51.6420° |
perigee height: | 414 km |
apogee height: | 422 km |
right ascension of ascending node: | 192.7535° |
argument of perigee: | 59.8797° |
revolutions per day: | 15.49641125 |
mean anomaly at epoch: | 75.3053° |
orbit number at epoch: | 41731 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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