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 64598U 26145.52123612 +.00000000 +00000-0 +88823-3 0 00007
2 64598 53.1616 338.6806 0001333 86.1314 273.9839 15.30219895 07
| Epoch (UTC): | 25 May 2026 12:30:34 |
| Eccentricity: | 0.0001333 |
| inclination: | 53.1616° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.6806° |
| argument of perigee: | 86.1314° |
| revolutions per day: | 15.30219895 |
| mean anomaly at epoch: | 273.9839° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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