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 59330U 26145.30383389 +.00000000 +00000-0 +60918-5 0 00007
2 59330 43.0025 114.6161 0000935 289.3233 70.7517 15.27577515 05
| Epoch (UTC): | 25 May 2026 07:17:31 |
| Eccentricity: | 0.0000935 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.6161° |
| argument of perigee: | 289.3233° |
| revolutions per day: | 15.27577515 |
| mean anomaly at epoch: | 70.7517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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