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 23405U 94077B 23275.81443228 .00000244 00000-0 14999-3 0 9997
2 23405 70.9823 62.1803 0000756 27.9183 332.1980 14.15328569490455
| Epoch (UTC): | 02 October 2023 19:32:46 |
| Eccentricity: | 0.0000756 |
| inclination: | 70.9823° |
| perigee height: | 840 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 62.1803° |
| argument of perigee: | 27.9183° |
| revolutions per day: | 14.15328569 |
| mean anomaly at epoch: | 332.1980° |
| orbit number at epoch: | 49045 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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