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 23030.22282150 .00015523 00000-0 27656-3 0 9995
2 25544 51.6435 291.8965 0004577 289.8386 208.1328 15.50288450380398
Epoch (UTC): | 30 January 2023 05:20:51 |
Eccentricity: | 0.0004577 |
inclination: | 51.6435° |
perigee height: | 413 km |
apogee height: | 419 km |
right ascension of ascending node: | 291.8965° |
argument of perigee: | 289.8386° |
revolutions per day: | 15.50288450 |
mean anomaly at epoch: | 208.1328° |
orbit number at epoch: | 38039 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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