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 23157.45225371 .00035147 00000-0 73650-3 0 9992
2 43137 97.3287 236.5330 0006654 167.8625 192.2785 15.45317348300653
| Epoch (UTC): | 06 June 2023 10:51:14 |
| Eccentricity: | 0.0006654 |
| inclination: | 97.3287° |
| perigee height: | 426 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 236.5330° |
| argument of perigee: | 167.8625° |
| revolutions per day: | 15.45317348 |
| mean anomaly at epoch: | 192.2785° |
| orbit number at epoch: | 30065 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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