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 39421U 13066F 23274.47109281 .00005420 00000-0 53857-3 0 9997
2 39421 97.5487 250.8976 0028856 172.7393 187.4250 14.91785552535332
Epoch (UTC): | 01 October 2023 11:18:22 |
Eccentricity: | 0.0028856 |
inclination: | 97.5487° |
perigee height: | 572 km |
apogee height: | 612 km |
right ascension of ascending node: | 250.8976° |
argument of perigee: | 172.7393° |
revolutions per day: | 14.91785552 |
mean anomaly at epoch: | 187.4250° |
orbit number at epoch: | 53533 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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