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 59642U 26145.08383961 +.00000000 +00000-0 -25729-5 0 00006
2 59642 43.0020 28.0002 0001405 271.9168 88.1522 15.27578817 00
| Epoch (UTC): | 25 May 2026 02:00:43 |
| Eccentricity: | 0.0001405 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 28.0002° |
| argument of perigee: | 271.9168° |
| revolutions per day: | 15.27578817 |
| mean anomaly at epoch: | 88.1522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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