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 64610U 26145.51385128 +.00000000 +00000-0 +56935-3 0 00002
2 64610 53.1583 338.6346 0001521 90.0431 270.0744 15.30204675 00
| Epoch (UTC): | 25 May 2026 12:19:56 |
| Eccentricity: | 0.0001521 |
| inclination: | 53.1583° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.6346° |
| argument of perigee: | 90.0431° |
| revolutions per day: | 15.30204675 |
| mean anomaly at epoch: | 270.0744° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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