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 39440U 13066AA 23331.83935777 .00004972 00000-0 62068-3 0 9994
2 39440 97.7921 275.5426 0071908 213.4215 146.2449 14.80992069538364
| Epoch (UTC): | 27 November 2023 20:08:40 |
| Eccentricity: | 0.0071908 |
| inclination: | 97.7921° |
| perigee height: | 576 km |
| apogee height: | 676 km |
| right ascension of ascending node: | 275.5426° |
| argument of perigee: | 213.4215° |
| revolutions per day: | 14.80992069 |
| mean anomaly at epoch: | 146.2449° |
| orbit number at epoch: | 53836 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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