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 64323U 26145.53013738 +.00000000 +00000-0 +15416-2 0 00008
2 64323 42.9997 285.6666 0002871 294.4870 65.5698 15.70816259 04
| Epoch (UTC): | 25 May 2026 12:43:23 |
| Eccentricity: | 0.0002871 |
| inclination: | 42.9997° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 285.6666° |
| argument of perigee: | 294.4870° |
| revolutions per day: | 15.70816259 |
| mean anomaly at epoch: | 65.5698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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