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 59802U 26145.40883634 +.00000000 +00000-0 +10709-3 0 00001
2 59802 43.0019 136.0369 0001439 276.5868 83.4820 15.27599379 02
| Epoch (UTC): | 25 May 2026 09:48:43 |
| Eccentricity: | 0.0001439 |
| inclination: | 43.0019° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 136.0369° |
| argument of perigee: | 276.5868° |
| revolutions per day: | 15.27599379 |
| mean anomaly at epoch: | 83.4820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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