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 56557U 26145.46468142 +.00000000 +00000-0 +18568-4 0 00006
2 56557 43.0048 150.0113 0001480 281.6471 78.4214 15.27576253 01
| Epoch (UTC): | 25 May 2026 11:09:08 |
| Eccentricity: | 0.0001480 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.0113° |
| argument of perigee: | 281.6471° |
| revolutions per day: | 15.27576253 |
| mean anomaly at epoch: | 78.4214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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