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 63587U 26145.34344649 +.00000000 +00000-0 +47569-3 0 00001
2 63587 43.0027 248.7887 0001691 268.0235 92.0423 15.27585046 07
| Epoch (UTC): | 25 May 2026 08:14:33 |
| Eccentricity: | 0.0001691 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 248.7887° |
| argument of perigee: | 268.0235° |
| revolutions per day: | 15.27585046 |
| mean anomaly at epoch: | 92.0423° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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