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 64465U 26145.27619344 +.00000000 +00000-0 +58474-3 0 00003
2 64465 53.1589 92.4493 0001197 93.6775 266.4364 15.34412541 05
| Epoch (UTC): | 25 May 2026 06:37:43 |
| Eccentricity: | 0.0001197 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.4493° |
| argument of perigee: | 93.6775° |
| revolutions per day: | 15.34412541 |
| mean anomaly at epoch: | 266.4364° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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