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 59786U 26145.35102169 +.00000000 +00000-0 +31062-5 0 00000
2 59786 43.0013 135.6251 0000975 279.5455 80.5287 15.27575538 07
| Epoch (UTC): | 25 May 2026 08:25:28 |
| Eccentricity: | 0.0000975 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.6251° |
| argument of perigee: | 279.5455° |
| revolutions per day: | 15.27575538 |
| mean anomaly at epoch: | 80.5287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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