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 64247U 26145.52468825 +.00000000 +00000-0 +76431-3 0 00008
2 64247 42.9995 232.8306 0001483 287.0099 73.0590 15.27597333 07
| Epoch (UTC): | 25 May 2026 12:35:33 |
| Eccentricity: | 0.0001483 |
| inclination: | 42.9995° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 232.8306° |
| argument of perigee: | 287.0099° |
| revolutions per day: | 15.27597333 |
| mean anomaly at epoch: | 73.0590° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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