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 43770U 18099N 25138.68402367 .00010770 00000-0 54994-3 0 9992
2 43770 97.4925 197.0164 0008952 289.2467 70.7797 15.16846037353233
Epoch (UTC): | 18 May 2025 16:24:59 |
Eccentricity: | 0.0008952 |
inclination: | 97.4925° |
perigee height: | 509 km |
apogee height: | 521 km |
right ascension of ascending node: | 197.0164° |
argument of perigee: | 289.2467° |
revolutions per day: | 15.16846037 |
mean anomaly at epoch: | 70.7797° |
orbit number at epoch: | 35323 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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