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 64227U 26145.02466899 +.00000000 +00000-0 +55092-3 0 00000
2 64227 53.1574 44.9743 0000834 70.7132 289.3959 15.30205550 05
| Epoch (UTC): | 25 May 2026 00:35:31 |
| Eccentricity: | 0.0000834 |
| inclination: | 53.1574° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 44.9743° |
| argument of perigee: | 70.7132° |
| revolutions per day: | 15.30205550 |
| mean anomaly at epoch: | 289.3959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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