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 63578U 26145.59985392 +.00000000 +00000-0 +63790-3 0 00008
2 63578 43.0011 247.2805 0001693 262.2284 97.8375 15.27589660 01
| Epoch (UTC): | 25 May 2026 14:23:47 |
| Eccentricity: | 0.0001693 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 247.2805° |
| argument of perigee: | 262.2284° |
| revolutions per day: | 15.27589660 |
| mean anomaly at epoch: | 97.8375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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