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 64175U 26145.15219478 +.00000000 +00000-0 +61803-3 0 00002
2 64175 53.1576 95.8442 0001139 83.7212 276.3919 15.31711986 00
| Epoch (UTC): | 25 May 2026 03:39:09 |
| Eccentricity: | 0.0001139 |
| inclination: | 53.1576° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 95.8442° |
| argument of perigee: | 83.7212° |
| revolutions per day: | 15.31711986 |
| mean anomaly at epoch: | 276.3919° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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