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 25133.88201195 .00012475 00000-0 61525-3 0 9992
2 32791 97.7268 113.3440 0001553 246.8758 113.2312 15.18066785926448
| Epoch (UTC): | 13 May 2025 21:10:05 |
| Eccentricity: | 0.0001553 |
| inclination: | 97.7268° |
| perigee height: | 510 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 113.3440° |
| argument of perigee: | 246.8758° |
| revolutions per day: | 15.18066785 |
| mean anomaly at epoch: | 113.2312° |
| orbit number at epoch: | 92644 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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