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 64085U 26145.01991925 +.00000000 +00000-0 +72081-3 0 00001
2 64085 43.0047 130.5199 0002751 290.3731 69.6825 15.27603757 00
| Epoch (UTC): | 25 May 2026 00:28:41 |
| Eccentricity: | 0.0002751 |
| inclination: | 43.0047° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 130.5199° |
| argument of perigee: | 290.3731° |
| revolutions per day: | 15.27603757 |
| mean anomaly at epoch: | 69.6825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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