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 39445U 13066AF 23333.39859695 .00007753 00000-0 81962-3 0 9990
2 39445 97.6965 292.0870 0053270 89.6887 271.0434 14.88423112540138
| Epoch (UTC): | 29 November 2023 09:33:58 |
| Eccentricity: | 0.0053270 |
| inclination: | 97.6965° |
| perigee height: | 565 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 292.0870° |
| argument of perigee: | 89.6887° |
| revolutions per day: | 14.88423112 |
| mean anomaly at epoch: | 271.0434° |
| orbit number at epoch: | 54013 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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