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 63647U 26145.45728074 +.00000000 +00000-0 +74667-3 0 00007
2 63647 42.9994 291.9995 0001564 272.9208 87.1464 15.27598021 05
| Epoch (UTC): | 25 May 2026 10:58:29 |
| Eccentricity: | 0.0001564 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 291.9995° |
| argument of perigee: | 272.9208° |
| revolutions per day: | 15.27598021 |
| mean anomaly at epoch: | 87.1464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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