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 32789U 08021G 23078.87186736 .00049631 00000-0 18786-2 0 9991
2 32789 97.3149 101.5504 0010207 88.7210 271.5199 15.26715489813718
| Epoch (UTC): | 19 March 2023 20:55:29 |
| Eccentricity: | 0.0010207 |
| inclination: | 97.3149° |
| perigee height: | 478 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 101.5504° |
| argument of perigee: | 88.7210° |
| revolutions per day: | 15.26715489 |
| mean anomaly at epoch: | 271.5199° |
| orbit number at epoch: | 81371 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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