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 64669U 26145.22708288 +.00000000 +00000-0 +81700-3 0 00008
2 64669 53.1596 130.7329 0000758 76.0952 284.0135 15.34400153 05
| Epoch (UTC): | 25 May 2026 05:26:59 |
| Eccentricity: | 0.0000758 |
| inclination: | 53.1596° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 130.7329° |
| argument of perigee: | 76.0952° |
| revolutions per day: | 15.34400153 |
| mean anomaly at epoch: | 284.0135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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