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 00020U 59007A 23037.90107200 .00003564 00000-0 14667-2 0 9991
2 00020 33.3490 344.5930 1660153 345.2364 10.4889 11.56689968342236
| Epoch (UTC): | 06 February 2023 21:37:32 |
| Eccentricity: | 0.1660153 |
| inclination: | 33.3490° |
| perigee height: | 509 km |
| apogee height: | 3252 km |
| right ascension of ascending node: | 344.5930° |
| argument of perigee: | 345.2364° |
| revolutions per day: | 11.56689968 |
| mean anomaly at epoch: | 10.4889° |
| orbit number at epoch: | 34223 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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