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 64687U 26145.33631311 +.00000000 +00000-0 +70906-3 0 00008
2 64687 53.1586 129.9902 0001134 87.1009 273.0123 15.34397295 03
| Epoch (UTC): | 25 May 2026 08:04:17 |
| Eccentricity: | 0.0001134 |
| inclination: | 53.1586° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 129.9902° |
| argument of perigee: | 87.1009° |
| revolutions per day: | 15.34397295 |
| mean anomaly at epoch: | 273.0123° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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