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 43010U 17072A 23033.54417260 .00000148 00000-0 92126-4 0 9992
2 43010 98.8450 342.2933 0001551 15.3094 344.8122 14.19137706270400
| Epoch (UTC): | 02 February 2023 13:03:36 |
| Eccentricity: | 0.0001551 |
| inclination: | 98.8450° |
| perigee height: | 827 km |
| apogee height: | 829 km |
| right ascension of ascending node: | 342.2933° |
| argument of perigee: | 15.3094° |
| revolutions per day: | 14.19137706 |
| mean anomaly at epoch: | 344.8122° |
| orbit number at epoch: | 27040 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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