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 59783U 26145.40032009 +.00000000 +00000-0 +29355-4 0 00009
2 59783 43.0005 132.4531 0000923 269.7767 90.2979 15.27577759 04
| Epoch (UTC): | 25 May 2026 09:36:27 |
| Eccentricity: | 0.0000923 |
| inclination: | 43.0005° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.4531° |
| argument of perigee: | 269.7767° |
| revolutions per day: | 15.27577759 |
| mean anomaly at epoch: | 90.2979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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