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 43223U 18021A 22228.98393326 0.00000000 00000-0 00000-0 0 08
2 43223 97.3539 348.0220 0002363 22.0899 337.9100 15.27648835 07
| Epoch (UTC): | 16 August 2022 23:36:51 |
| Eccentricity: | 0.0002363 |
| inclination: | 97.3539° |
| perigee height: | 481 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 348.0220° |
| argument of perigee: | 22.0899° |
| revolutions per day: | 15.27648835 |
| mean anomaly at epoch: | 337.9100° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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