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 is defined by the following mean orbital elements,
1 63152U 26144.93438875 +.00000000 +00000-0 +92500-3 0 00003
2 63152 43.0015 312.4660 0002072 275.4678 84.5937 15.27608914 03
| Epoch (UTC): | 24 May 2026 22:25:31 |
| Eccentricity: | 0.0002072 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 312.4660° |
| argument of perigee: | 275.4678° |
| revolutions per day: | 15.27608914 |
| mean anomaly at epoch: | 84.5937° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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