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 43138U 18004AD 23140.07319936 .18079883 25453-5 20639-3 0 9991
2 43138 97.3024 230.4644 0016113 279.5975 80.3508 16.49267352298665
| Epoch (UTC): | 20 May 2023 01:45:24 |
| Eccentricity: | 0.0016113 |
| inclination: | 97.3024° |
| perigee height: | 131 km |
| apogee height: | 152 km |
| right ascension of ascending node: | 230.4644° |
| argument of perigee: | 279.5975° |
| revolutions per day: | 16.49267352 |
| mean anomaly at epoch: | 80.3508° |
| orbit number at epoch: | 29866 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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