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 5560U 71089A 25197.21294328 .00000249 00000-0 63948-4 0 9995
2 5560 92.7205 75.2694 0016478 155.3174 204.8823 14.50424583828302
| Epoch (UTC): | 16 July 2025 05:06:38 |
| Eccentricity: | 0.0016478 |
| inclination: | 92.7205° |
| perigee height: | 712 km |
| apogee height: | 736 km |
| right ascension of ascending node: | 75.2694° |
| argument of perigee: | 155.3174° |
| revolutions per day: | 14.50424583 |
| mean anomaly at epoch: | 204.8823° |
| orbit number at epoch: | 82830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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