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 64238U 26145.26265006 +.00000000 +00000-0 +12465-2 0 00001
2 64238 42.9998 107.9167 0001748 275.6978 84.3691 15.70895825 02
| Epoch (UTC): | 25 May 2026 06:18:12 |
| Eccentricity: | 0.0001748 |
| inclination: | 42.9998° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 107.9167° |
| argument of perigee: | 275.6978° |
| revolutions per day: | 15.70895825 |
| mean anomaly at epoch: | 84.3691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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