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 23238.98397791 0.00000000 00000-0 00000-0 0 00
2 43223 97.3536 357.6624 0002709 39.5167 320.4831 15.27655102 06
| Epoch (UTC): | 26 August 2023 23:36:55 |
| Eccentricity: | 0.0002709 |
| inclination: | 97.3536° |
| perigee height: | 481 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 357.6624° |
| argument of perigee: | 39.5167° |
| revolutions per day: | 15.27655102 |
| mean anomaly at epoch: | 320.4831° |
| 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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