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 47956U 21022AA 23266.93533266 .00016648 00000-0 87134-3 0 9995
2 47956 97.4834 162.7989 0018347 1.6700 358.4591 15.15757477137765
| Epoch (UTC): | 23 September 2023 22:26:52 |
| Eccentricity: | 0.0018347 |
| inclination: | 97.4834° |
| perigee height: | 506 km |
| apogee height: | 531 km |
| right ascension of ascending node: | 162.7989° |
| argument of perigee: | 1.6700° |
| revolutions per day: | 15.15757477 |
| mean anomaly at epoch: | 358.4591° |
| orbit number at epoch: | 13776 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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