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 64233U 26145.25825292 +.00000000 +00000-0 +13188-2 0 00007
2 64233 43.0014 107.8825 0002072 275.6433 84.4198 15.70881128 09
| Epoch (UTC): | 25 May 2026 06:11:53 |
| Eccentricity: | 0.0002072 |
| inclination: | 43.0014° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 107.8825° |
| argument of perigee: | 275.6433° |
| revolutions per day: | 15.70881128 |
| mean anomaly at epoch: | 84.4198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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