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 23340.48651887 .00014051 00000-0 25175-3 0 9993
2 25544 51.6416 195.1287 0001458 11.2264 61.5007 15.50224296428517
Epoch (UTC): | 06 December 2023 11:40:35 |
Eccentricity: | 0.0001458 |
inclination: | 51.6416° |
perigee height: | 415 km |
apogee height: | 417 km |
right ascension of ascending node: | 195.1287° |
argument of perigee: | 11.2264° |
revolutions per day: | 15.50224296 |
mean anomaly at epoch: | 61.5007° |
orbit number at epoch: | 42851 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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