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 39444U 13066AE 23333.86643474 .00009113 00000-0 95469-3 0 9996
2 39444 97.6951 292.8185 0053097 85.3360 275.3919 14.88741522540868
| Epoch (UTC): | 29 November 2023 20:47:39 |
| Eccentricity: | 0.0053097 |
| inclination: | 97.6951° |
| perigee height: | 565 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 292.8185° |
| argument of perigee: | 85.3360° |
| revolutions per day: | 14.88741522 |
| mean anomaly at epoch: | 275.3919° |
| orbit number at epoch: | 54086 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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