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 64464U 26145.23832116 +.00000000 +00000-0 +69251-3 0 00007
2 64464 53.1592 92.2162 0000885 101.1691 258.9412 15.34404271 05
| Epoch (UTC): | 25 May 2026 05:43:10 |
| Eccentricity: | 0.0000885 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.2162° |
| argument of perigee: | 101.1691° |
| revolutions per day: | 15.34404271 |
| mean anomaly at epoch: | 258.9412° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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