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 64097U 26145.39184233 +.00000000 +00000-0 +79135-3 0 00008
2 64097 53.1604 29.9487 0001267 92.5806 267.5341 15.34405384 07
| Epoch (UTC): | 25 May 2026 09:24:15 |
| Eccentricity: | 0.0001267 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 29.9487° |
| argument of perigee: | 92.5806° |
| revolutions per day: | 15.34405384 |
| mean anomaly at epoch: | 267.5341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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