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 43137U 18004AC 23088.70802359 .00043076 00000-0 10649-2 0 9998
2 43137 97.3337 167.3518 0006554 76.3746 283.8230 15.40326579290050
Epoch (UTC): | 29 March 2023 16:59:33 |
Eccentricity: | 0.0006554 |
inclination: | 97.3337° |
perigee height: | 440 km |
apogee height: | 449 km |
right ascension of ascending node: | 167.3518° |
argument of perigee: | 76.3746° |
revolutions per day: | 15.40326579 |
mean anomaly at epoch: | 283.8230° |
orbit number at epoch: | 29005 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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