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 59573U 26145.12343793 +.00000000 +00000-0 +40101-4 0 00002
2 59573 42.9998 297.2187 0001149 276.6297 83.4424 15.27575916 05
| Epoch (UTC): | 25 May 2026 02:57:45 |
| Eccentricity: | 0.0001149 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 297.2187° |
| argument of perigee: | 276.6297° |
| revolutions per day: | 15.27575916 |
| mean anomaly at epoch: | 83.4424° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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