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 59633U 26145.18882601 +.00000000 +00000-0 +21735-4 0 00003
2 59633 43.0005 60.6643 0000869 272.0844 87.9908 15.27574768 08
| Epoch (UTC): | 25 May 2026 04:31:54 |
| Eccentricity: | 0.0000869 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 60.6643° |
| argument of perigee: | 272.0844° |
| revolutions per day: | 15.27574768 |
| mean anomaly at epoch: | 87.9908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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