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 43937U 19003F 23313.54107761 .16492241 25339-5 26604-3 0 9999
2 43937 97.0315 342.1459 0005268 231.7168 128.3663 16.48231493268837
Epoch (UTC): | 09 November 2023 12:59:09 |
Eccentricity: | 0.0005268 |
inclination: | 97.0315° |
perigee height: | 140 km |
apogee height: | 147 km |
right ascension of ascending node: | 342.1459° |
argument of perigee: | 231.7168° |
revolutions per day: | 16.48231493 |
mean anomaly at epoch: | 128.3663° |
orbit number at epoch: | 26883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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