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 56522U 26145.29294455 +.00000000 +00000-0 +26412-4 0 00000
2 56522 42.9995 139.9919 0001353 279.7324 80.3375 15.27575399 06
| Epoch (UTC): | 25 May 2026 07:01:50 |
| Eccentricity: | 0.0001353 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.9919° |
| argument of perigee: | 279.7324° |
| revolutions per day: | 15.27575399 |
| mean anomaly at epoch: | 80.3375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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