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 20323U 89089B 23151.95962001 .00000505 00000-0 13785-3 0 9995
2 20323 97.0679 142.2472 0072824 76.8900 284.0412 14.48871839748996
| Epoch (UTC): | 31 May 2023 23:01:51 |
| Eccentricity: | 0.0072824 |
| inclination: | 97.0679° |
| perigee height: | 677 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 142.2472° |
| argument of perigee: | 76.8900° |
| revolutions per day: | 14.48871839 |
| mean anomaly at epoch: | 284.0412° |
| orbit number at epoch: | 74899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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