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 63748U 26145.38920566 +.00000000 +00000-0 +13143-3 0 00003
2 63748 51.8995 133.9243 0000763 27.3940 332.7062 14.79932469 00
| Epoch (UTC): | 25 May 2026 09:20:27 |
| Eccentricity: | 0.0000763 |
| inclination: | 51.8995° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 133.9243° |
| argument of perigee: | 27.3940° |
| revolutions per day: | 14.79932469 |
| mean anomaly at epoch: | 332.7062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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