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 25860U 99039A 23152.85008345 .00000776 00000-0 11613-3 0 9992
2 25860 98.0896 199.8533 0001565 73.4165 286.7216 14.77504520284836
Epoch (UTC): | 01 June 2023 20:24:07 |
Eccentricity: | 0.0001565 |
inclination: | 98.0896° |
perigee height: | 636 km |
apogee height: | 638 km |
right ascension of ascending node: | 199.8533° |
argument of perigee: | 73.4165° |
revolutions per day: | 14.77504520 |
mean anomaly at epoch: | 286.7216° |
orbit number at epoch: | 28483 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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