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 23270.09434028 .00025309 00000-0 45380-3 0 9996
2 25544 51.6415 183.7622 0005410 63.3024 128.5013 15.49751646417595
Epoch (UTC): | 27 September 2023 02:15:51 |
Eccentricity: | 0.0005410 |
inclination: | 51.6415° |
perigee height: | 414 km |
apogee height: | 421 km |
right ascension of ascending node: | 183.7622° |
argument of perigee: | 63.3024° |
revolutions per day: | 15.49751646 |
mean anomaly at epoch: | 128.5013° |
orbit number at epoch: | 41759 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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