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 64004U 26145.64662042 +.00000000 +00000-0 +64328-3 0 00001
2 64004 43.0002 283.4506 0000538 270.7171 89.3619 15.27600834 06
| Epoch (UTC): | 25 May 2026 15:31:08 |
| Eccentricity: | 0.0000538 |
| inclination: | 43.0002° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 283.4506° |
| argument of perigee: | 270.7171° |
| revolutions per day: | 15.27600834 |
| mean anomaly at epoch: | 89.3619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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