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 56512U 26145.45698257 +.00000000 +00000-0 +11542-3 0 00002
2 56512 43.0034 138.6452 0001229 272.4345 87.6367 15.27595500 01
| Epoch (UTC): | 25 May 2026 10:58:03 |
| Eccentricity: | 0.0001229 |
| inclination: | 43.0034° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.6452° |
| argument of perigee: | 272.4345° |
| revolutions per day: | 15.27595500 |
| mean anomaly at epoch: | 87.6367° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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