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 56537U 26145.66668980 +.00000000 +00000-0 -60162-3 0 00005
2 56537 43.0010 151.9649 0001610 271.4772 257.8260 15.27578109 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001610 |
| inclination: | 43.0010° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 151.9649° |
| argument of perigee: | 271.4772° |
| revolutions per day: | 15.27578109 |
| mean anomaly at epoch: | 257.8260° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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