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 28931U 06002A 24306.85843258 .00006740 00000-0 12088-2 0 9997
2 28931 98.0539 257.1938 0002581 76.3963 283.7529 14.67061912 1525
Epoch (UTC): | 01 November 2024 20:36:08 |
Eccentricity: | 0.0002581 |
inclination: | 98.0539° |
perigee height: | 668 km |
apogee height: | 672 km |
right ascension of ascending node: | 257.1938° |
argument of perigee: | 76.3963° |
revolutions per day: | 14.67061912 |
mean anomaly at epoch: | 283.7529° |
orbit number at epoch: | 152 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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