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 59794U 26145.37286372 +.00000000 +00000-0 +41550-4 0 00002
2 59794 43.0025 135.7822 0001470 270.1449 89.9234 15.27579552 00
| Epoch (UTC): | 25 May 2026 08:56:55 |
| Eccentricity: | 0.0001470 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.7822° |
| argument of perigee: | 270.1449° |
| revolutions per day: | 15.27579552 |
| mean anomaly at epoch: | 89.9234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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