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 64675U 26145.33570389 +.00000000 +00000-0 +32490-3 0 00008
2 64675 53.1575 131.4037 0001279 92.3817 267.7330 15.30200625 06
| Epoch (UTC): | 25 May 2026 08:03:24 |
| Eccentricity: | 0.0001279 |
| inclination: | 53.1575° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.4037° |
| argument of perigee: | 92.3817° |
| revolutions per day: | 15.30200625 |
| mean anomaly at epoch: | 267.7330° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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