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 63995U 26145.43889616 +.00000000 +00000-0 +51526-3 0 00000
2 63995 42.9979 284.4755 0000660 234.0053 126.0737 15.27596497 09
| Epoch (UTC): | 25 May 2026 10:32:00 |
| Eccentricity: | 0.0000660 |
| inclination: | 42.9979° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 284.4755° |
| argument of perigee: | 234.0053° |
| revolutions per day: | 15.27596497 |
| mean anomaly at epoch: | 126.0737° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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