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 64242U 26144.91287831 +.00000000 +00000-0 +16629-2 0 00003
2 64242 42.9980 109.5750 0002885 282.2409 77.8135 15.70989221 04
| Epoch (UTC): | 24 May 2026 21:54:32 |
| Eccentricity: | 0.0002885 |
| inclination: | 42.9980° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 109.5750° |
| argument of perigee: | 282.2409° |
| revolutions per day: | 15.70989221 |
| mean anomaly at epoch: | 77.8135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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