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 64731U 26145.49227264 +.00000000 +00000-0 +37244-3 0 00001
2 64731 53.1577 184.0905 0001098 78.4443 281.6681 15.30206777 06
| Epoch (UTC): | 25 May 2026 11:48:52 |
| Eccentricity: | 0.0001098 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.0905° |
| argument of perigee: | 78.4443° |
| revolutions per day: | 15.30206777 |
| mean anomaly at epoch: | 281.6681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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