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 27939U 03042A 23332.59215373 .00002513 00000-0 43672-3 0 9993
2 27939 98.2642 121.0890 0011884 342.5671 86.1213 14.69024995 78548
| Epoch (UTC): | 28 November 2023 14:12:42 |
| Eccentricity: | 0.0011884 |
| inclination: | 98.2642° |
| perigee height: | 656 km |
| apogee height: | 672 km |
| right ascension of ascending node: | 121.0890° |
| argument of perigee: | 342.5671° |
| revolutions per day: | 14.69024995 |
| mean anomaly at epoch: | 86.1213° |
| orbit number at epoch: | 7854 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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