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 47688U 21006EP 23331.91755748 .00030390 00000-0 86166-3 0 9995
2 47688 97.3667 30.0016 0006530 189.7560 170.3558 15.36169835158744
| Epoch (UTC): | 27 November 2023 22:01:16 |
| Eccentricity: | 0.0006530 |
| inclination: | 97.3667° |
| perigee height: | 453 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 30.0016° |
| argument of perigee: | 189.7560° |
| revolutions per day: | 15.36169835 |
| mean anomaly at epoch: | 170.3558° |
| orbit number at epoch: | 15874 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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