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 23086.75901039 .00036774 00000-0 91502-3 0 9991
2 43137 97.3338 165.3972 0006633 82.4555 277.7444 15.40162916289754
| Epoch (UTC): | 27 March 2023 18:12:58 |
| Eccentricity: | 0.0006633 |
| inclination: | 97.3338° |
| perigee height: | 441 km |
| apogee height: | 450 km |
| right ascension of ascending node: | 165.3972° |
| argument of perigee: | 82.4555° |
| revolutions per day: | 15.40162916 |
| mean anomaly at epoch: | 277.7444° |
| orbit number at epoch: | 28975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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