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 56338U 26144.96506124 +.00000000 +00000-0 -32582-4 0 00003
2 56338 97.4473 144.9626 0002619 110.5082 249.6426 15.05658073 01
| Epoch (UTC): | 24 May 2026 23:09:41 |
| Eccentricity: | 0.0002619 |
| inclination: | 97.4473° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 144.9626° |
| argument of perigee: | 110.5082° |
| revolutions per day: | 15.05658073 |
| mean anomaly at epoch: | 249.6426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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