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 56513U 26145.34034337 +.00000000 +00000-0 +14087-4 0 00002
2 56513 43.0009 139.4961 0001163 268.2105 91.8613 15.27575733 09
| Epoch (UTC): | 25 May 2026 08:10:05 |
| Eccentricity: | 0.0001163 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.4961° |
| argument of perigee: | 268.2105° |
| revolutions per day: | 15.27575733 |
| mean anomaly at epoch: | 91.8613° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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