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 43793U 18099AM 25138.79428187 .00166563 00000-0 15408-2 0 9995
2 43793 97.4822 215.1379 0007756 200.5874 159.5075 15.66974744354220
Epoch (UTC): | 18 May 2025 19:03:45 |
Eccentricity: | 0.0007756 |
inclination: | 97.4822° |
perigee height: | 362 km |
apogee height: | 373 km |
right ascension of ascending node: | 215.1379° |
argument of perigee: | 200.5874° |
revolutions per day: | 15.66974744 |
mean anomaly at epoch: | 159.5075° |
orbit number at epoch: | 35422 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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