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 64390U 26145.37908841 +.00000000 +00000-0 +78333-3 0 00000
2 64390 42.9999 106.8552 0001108 277.0617 83.0108 15.27602305 04
| Epoch (UTC): | 25 May 2026 09:05:53 |
| Eccentricity: | 0.0001108 |
| inclination: | 42.9999° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 106.8552° |
| argument of perigee: | 277.0617° |
| revolutions per day: | 15.27602305 |
| mean anomaly at epoch: | 83.0108° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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