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 59317U 26145.37783226 +.00000000 +00000-0 +24313-4 0 00001
2 59317 43.0015 157.5370 0001297 271.6731 88.3972 15.27578856 05
| Epoch (UTC): | 25 May 2026 09:04:04 |
| Eccentricity: | 0.0001297 |
| inclination: | 43.0015° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 157.5370° |
| argument of perigee: | 271.6731° |
| revolutions per day: | 15.27578856 |
| mean anomaly at epoch: | 88.3972° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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