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 63725U 26145.32975939 +.00000000 +00000-0 +20158-3 0 00000
2 63725 51.9019 126.7251 0000297 40.3776 319.7208 14.79952569 06
| Epoch (UTC): | 25 May 2026 07:54:51 |
| Eccentricity: | 0.0000297 |
| inclination: | 51.9019° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 126.7251° |
| argument of perigee: | 40.3776° |
| revolutions per day: | 14.79952569 |
| mean anomaly at epoch: | 319.7208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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