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 43678U 18084H 22178.77630926 .00000274 00000-0 32716-4 0 9995
2 43678 97.9719 312.1631 0008486 248.9063 111.1252 14.92183873199397
Epoch (UTC): | 27 June 2022 18:37:53 |
Eccentricity: | 0.0008486 |
inclination: | 97.9719° |
perigee height: | 585 km |
apogee height: | 597 km |
right ascension of ascending node: | 312.1631° |
argument of perigee: | 248.9063° |
revolutions per day: | 14.92183873 |
mean anomaly at epoch: | 111.1252° |
orbit number at epoch: | 19939 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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