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 63512U 26145.26199462 +.00000000 +00000-0 +55021-3 0 00003
2 63512 53.1598 144.2018 0001148 88.5234 271.5899 15.31728128 03
| Epoch (UTC): | 25 May 2026 06:17:16 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 144.2018° |
| argument of perigee: | 88.5234° |
| revolutions per day: | 15.31728128 |
| mean anomaly at epoch: | 271.5899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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