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 64596U 26145.50435375 +.00000000 +00000-0 +60912-3 0 00004
2 64596 53.1586 338.5787 0001527 86.7888 273.3287 15.30210226 05
| Epoch (UTC): | 25 May 2026 12:06:16 |
| Eccentricity: | 0.0001527 |
| inclination: | 53.1586° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 338.5787° |
| argument of perigee: | 86.7888° |
| revolutions per day: | 15.30210226 |
| mean anomaly at epoch: | 273.3287° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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