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 43445U 18036E 23030.42632375 -.00000031 00000-0 00000-0 0 9993
2 43445 4.0848 81.1179 0008606 120.2142 285.6795 1.02113631 14347
| Epoch (UTC): | 30 January 2023 10:13:54 |
| Eccentricity: | 0.0008606 |
| inclination: | 4.0848° |
| perigee height: | 35242 km |
| apogee height: | 35313 km |
| right ascension of ascending node: | 81.1179° |
| argument of perigee: | 120.2142° |
| revolutions per day: | 1.02113631 |
| mean anomaly at epoch: | 285.6795° |
| orbit number at epoch: | 1434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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