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 23089.74740956 .00047561 00000-0 11712-2 0 9992
2 43137 97.3337 168.3941 0006512 73.1215 287.0745 15.40422177290206
| Epoch (UTC): | 30 March 2023 17:56:16 |
| Eccentricity: | 0.0006512 |
| inclination: | 97.3337° |
| perigee height: | 440 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 168.3941° |
| argument of perigee: | 73.1215° |
| revolutions per day: | 15.40422177 |
| mean anomaly at epoch: | 287.0745° |
| orbit number at epoch: | 29020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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