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 56304U 26145.33053044 +.00000000 +00000-0 +17881-3 0 00009
2 56304 43.0002 135.7964 0001182 275.6182 84.4535 15.27591006 02
| Epoch (UTC): | 25 May 2026 07:55:57 |
| Eccentricity: | 0.0001182 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.7964° |
| argument of perigee: | 275.6182° |
| revolutions per day: | 15.27591006 |
| mean anomaly at epoch: | 84.4535° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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