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 59434U 26145.11963703 +.00000000 +00000-0 +33263-5 0 00008
2 59434 53.1612 288.6226 0001139 91.8700 268.2431 15.30194664 03
| Epoch (UTC): | 25 May 2026 02:52:16 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 288.6226° |
| argument of perigee: | 91.8700° |
| revolutions per day: | 15.30194664 |
| mean anomaly at epoch: | 268.2431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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