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 23334.87461333 .00008267 00000-0 86649-3 0 9999
2 39444 97.6953 293.7978 0053044 82.1959 278.5276 14.88757402541014
| Epoch (UTC): | 30 November 2023 20:59:26 |
| Eccentricity: | 0.0053044 |
| inclination: | 97.6953° |
| perigee height: | 565 km |
| apogee height: | 639 km |
| right ascension of ascending node: | 293.7978° |
| argument of perigee: | 82.1959° |
| revolutions per day: | 14.88757402 |
| mean anomaly at epoch: | 278.5276° |
| orbit number at epoch: | 54101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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