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 56518U 26145.47882256 +.00000000 +00000-0 -64898-5 0 00009
2 56518 43.0003 138.8150 0000976 267.9407 92.1332 15.27581510 05
| Epoch (UTC): | 25 May 2026 11:29:30 |
| Eccentricity: | 0.0000976 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 138.8150° |
| argument of perigee: | 267.9407° |
| revolutions per day: | 15.27581510 |
| mean anomaly at epoch: | 92.1332° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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