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 59747U 26145.33243749 +.00000000 +00000-0 +26109-4 0 00000
2 59747 43.0004 110.4853 0000975 271.1644 88.9096 15.27576067 09
| Epoch (UTC): | 25 May 2026 07:58:42 |
| Eccentricity: | 0.0000975 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 110.4853° |
| argument of perigee: | 271.1644° |
| revolutions per day: | 15.27576067 |
| mean anomaly at epoch: | 88.9096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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