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 59338U 26145.37949788 +.00000000 +00000-0 +45230-4 0 00002
2 59338 43.0027 114.3248 0001331 277.0250 83.0450 15.27575160 09
| Epoch (UTC): | 25 May 2026 09:06:28 |
| Eccentricity: | 0.0001331 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.3248° |
| argument of perigee: | 277.0250° |
| revolutions per day: | 15.27575160 |
| mean anomaly at epoch: | 83.0450° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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