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 56510U 26145.45313235 +.00000000 +00000-0 +20888-4 0 00004
2 56510 43.0039 138.6286 0001602 266.4840 93.5828 15.27578240 07
| Epoch (UTC): | 25 May 2026 10:52:30 |
| Eccentricity: | 0.0001602 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.6286° |
| argument of perigee: | 266.4840° |
| revolutions per day: | 15.27578240 |
| mean anomaly at epoch: | 93.5828° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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