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 32791U 08021J 25143.70255443 .00010295 00000-0 50507-3 0 9995
2 32791 97.7263 123.3736 0002714 191.2720 168.8453 15.18300942928017
| Epoch (UTC): | 23 May 2025 16:51:40 |
| Eccentricity: | 0.0002714 |
| inclination: | 97.7263° |
| perigee height: | 509 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 123.3736° |
| argument of perigee: | 191.2720° |
| revolutions per day: | 15.18300942 |
| mean anomaly at epoch: | 168.8453° |
| orbit number at epoch: | 92801 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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