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 63256U 26145.41449712 +.00000000 +00000-0 +78088-4 0 00000
2 63256 97.6990 37.0838 0001608 61.6054 298.5327 14.92877251 02
| Epoch (UTC): | 25 May 2026 09:56:52 |
| Eccentricity: | 0.0001608 |
| inclination: | 97.6990° |
| perigee height: | 588 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 37.0838° |
| argument of perigee: | 61.6054° |
| revolutions per day: | 14.92877251 |
| mean anomaly at epoch: | 298.5327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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