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 63519U 26145.40628596 +.00000000 +00000-0 +96969-3 0 00007
2 63519 53.1589 145.8115 0001198 85.2153 274.8984 15.30203953 08
| Epoch (UTC): | 25 May 2026 09:45:03 |
| Eccentricity: | 0.0001198 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 145.8115° |
| argument of perigee: | 85.2153° |
| revolutions per day: | 15.30203953 |
| mean anomaly at epoch: | 274.8984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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