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 63900U 26144.98339774 +.00000000 +00000-0 +90131-3 0 00005
2 63900 42.9973 105.5483 0000698 260.0196 100.0577 15.27591945 05
| Epoch (UTC): | 24 May 2026 23:36:05 |
| Eccentricity: | 0.0000698 |
| inclination: | 42.9973° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 105.5483° |
| argument of perigee: | 260.0196° |
| revolutions per day: | 15.27591945 |
| mean anomaly at epoch: | 100.0577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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