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 64455U 26145.11857275 +.00000000 +00000-0 +79595-3 0 00009
2 64455 53.1597 92.8977 0001149 78.0255 282.0876 15.34397636 00
| Epoch (UTC): | 25 May 2026 02:50:44 |
| Eccentricity: | 0.0001149 |
| inclination: | 53.1597° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.8977° |
| argument of perigee: | 78.0255° |
| revolutions per day: | 15.34397636 |
| mean anomaly at epoch: | 282.0876° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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