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 64908U 26145.53608957 +.00000000 +00000-0 +48516-3 0 00008
2 64908 53.1600 348.4159 0000823 109.2264 250.8826 15.31712101 08
| Epoch (UTC): | 25 May 2026 12:51:58 |
| Eccentricity: | 0.0000823 |
| inclination: | 53.1600° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 348.4159° |
| argument of perigee: | 109.2264° |
| revolutions per day: | 15.31712101 |
| mean anomaly at epoch: | 250.8826° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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