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 56519U 26145.36218613 +.00000000 +00000-0 +16645-4 0 00003
2 56519 43.0033 139.6481 0001187 314.5166 45.5589 15.27575869 07
| Epoch (UTC): | 25 May 2026 08:41:32 |
| Eccentricity: | 0.0001187 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.6481° |
| argument of perigee: | 314.5166° |
| revolutions per day: | 15.27575869 |
| mean anomaly at epoch: | 45.5589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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