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 60475U 26145.45682949 +.00000000 +00000-0 +16316-3 0 00000
2 60475 97.3736 221.8950 0002856 20.1086 340.0263 15.23346275 00
| Epoch (UTC): | 25 May 2026 10:57:50 |
| Eccentricity: | 0.0002856 |
| inclination: | 97.3736° |
| perigee height: | 494 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 221.8950° |
| argument of perigee: | 20.1086° |
| revolutions per day: | 15.23346275 |
| mean anomaly at epoch: | 340.0263° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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