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 59801U 26145.45240139 +.00000000 +00000-0 +28779-5 0 00000
2 59801 43.0002 135.5175 0000961 265.7187 94.3555 15.27577965 08
| Epoch (UTC): | 25 May 2026 10:51:27 |
| Eccentricity: | 0.0000961 |
| inclination: | 43.0002° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 135.5175° |
| argument of perigee: | 265.7187° |
| revolutions per day: | 15.27577965 |
| mean anomaly at epoch: | 94.3555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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