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 43440U 18040B 23343.11780026 .00014139 00000-0 39973-3 0 9990
2 43440 97.1682 28.8795 0006611 298.7820 61.2760 15.36414246312081
| Epoch (UTC): | 09 December 2023 02:49:37 |
| Eccentricity: | 0.0006611 |
| inclination: | 97.1682° |
| perigee height: | 452 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 28.8795° |
| argument of perigee: | 298.7820° |
| revolutions per day: | 15.36414246 |
| mean anomaly at epoch: | 61.2760° |
| orbit number at epoch: | 31208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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