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 43804U 18099AY 25138.71650373 .00012068 00000-0 59594-3 0 9999
2 43804 97.4734 197.3521 0011834 217.0102 143.0317 15.17962693353383
Epoch (UTC): | 18 May 2025 17:11:45 |
Eccentricity: | 0.0011834 |
inclination: | 97.4734° |
perigee height: | 504 km |
apogee height: | 520 km |
right ascension of ascending node: | 197.3521° |
argument of perigee: | 217.0102° |
revolutions per day: | 15.17962693 |
mean anomaly at epoch: | 143.0317° |
orbit number at epoch: | 35338 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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