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 59438U 26145.64479749 +.00000000 +00000-0 +15135-3 0 00008
2 59438 53.1616 284.0803 0000751 77.7958 282.3127 15.30190876 09
| Epoch (UTC): | 25 May 2026 15:28:30 |
| Eccentricity: | 0.0000751 |
| inclination: | 53.1616° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 284.0803° |
| argument of perigee: | 77.7958° |
| revolutions per day: | 15.30190876 |
| mean anomaly at epoch: | 282.3127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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