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 56503U 26145.46341045 +.00000000 +00000-0 -10172-4 0 00003
2 56503 43.0025 138.7071 0001428 269.0443 91.0245 15.27575996 02
| Epoch (UTC): | 25 May 2026 11:07:18 |
| Eccentricity: | 0.0001428 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.7071° |
| argument of perigee: | 269.0443° |
| revolutions per day: | 15.27575996 |
| mean anomaly at epoch: | 91.0245° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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