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 43156U 18008B 23276.53561903 .00039045 00000-0 12774-2 0 9992
2 43156 97.2896 327.0328 0007627 285.2559 74.7840 15.31563620315130
| Epoch (UTC): | 03 October 2023 12:51:17 |
| Eccentricity: | 0.0007627 |
| inclination: | 97.2896° |
| perigee height: | 466 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 327.0328° |
| argument of perigee: | 285.2559° |
| revolutions per day: | 15.31563620 |
| mean anomaly at epoch: | 74.7840° |
| orbit number at epoch: | 31513 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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