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 59210U 26145.47012348 +.00000000 +00000-0 +31295-4 0 00001
2 59210 53.1591 158.7933 0001061 85.0634 275.0488 15.30194735 05
| Epoch (UTC): | 25 May 2026 11:16:58 |
| Eccentricity: | 0.0001061 |
| inclination: | 53.1591° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 158.7933° |
| argument of perigee: | 85.0634° |
| revolutions per day: | 15.30194735 |
| mean anomaly at epoch: | 275.0488° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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