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 23090.19783697 -.00125339 00000-0 -22800-2 0 9993
2 25544 51.6417 354.9554 0007332 134.3235 356.4299 15.49256375389697
Epoch (UTC): | 31 March 2023 04:44:53 |
Eccentricity: | 0.0007332 |
inclination: | 51.6417° |
perigee height: | 414 km |
apogee height: | 424 km |
right ascension of ascending node: | 354.9554° |
argument of perigee: | 134.3235° |
revolutions per day: | 15.49256375 |
mean anomaly at epoch: | 356.4299° |
orbit number at epoch: | 38969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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