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 59804U 26145.46009738 +.00000000 +00000-0 -14938-3 0 00003
2 59804 43.0007 135.5752 0001278 271.1532 88.9173 15.27584754 03
| Epoch (UTC): | 25 May 2026 11:02:32 |
| Eccentricity: | 0.0001278 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.5752° |
| argument of perigee: | 271.1532° |
| revolutions per day: | 15.27584754 |
| mean anomaly at epoch: | 88.9173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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