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 23151.43505870 .00004439 00000-0 49488-3 0 9990
2 39444 97.6700 116.2221 0052239 329.9543 29.8679 14.86557350513741
| Epoch (UTC): | 31 May 2023 10:26:29 |
| Eccentricity: | 0.0052239 |
| inclination: | 97.6700° |
| perigee height: | 572 km |
| apogee height: | 645 km |
| right ascension of ascending node: | 116.2221° |
| argument of perigee: | 329.9543° |
| revolutions per day: | 14.86557350 |
| mean anomaly at epoch: | 29.8679° |
| orbit number at epoch: | 51374 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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