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 32787U 08021E 25143.95035351 .00042017 00000-0 93302-3 0 9998
2 32787 97.6431 133.3349 0008524 88.1802 272.0422 15.43549597929686
| Epoch (UTC): | 23 May 2025 22:48:30 |
| Eccentricity: | 0.0008524 |
| inclination: | 97.6431° |
| perigee height: | 430 km |
| apogee height: | 441 km |
| right ascension of ascending node: | 133.3349° |
| argument of perigee: | 88.1802° |
| revolutions per day: | 15.43549597 |
| mean anomaly at epoch: | 272.0422° |
| orbit number at epoch: | 92968 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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