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 64667U 26145.39363146 +.00000000 +00000-0 +50939-3 0 00004
2 64667 53.1568 131.0576 0001483 67.0508 293.0649 15.30209354 09
| Epoch (UTC): | 25 May 2026 09:26:49 |
| Eccentricity: | 0.0001483 |
| inclination: | 53.1568° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 131.0576° |
| argument of perigee: | 67.0508° |
| revolutions per day: | 15.30209354 |
| mean anomaly at epoch: | 293.0649° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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