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 59325U 26145.38335351 +.00000000 +00000-0 -31975-6 0 00008
2 59325 43.0013 114.3582 0001314 274.8033 85.2669 15.27576941 00
| Epoch (UTC): | 25 May 2026 09:12:01 |
| Eccentricity: | 0.0001314 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.3582° |
| argument of perigee: | 274.8033° |
| revolutions per day: | 15.27576941 |
| mean anomaly at epoch: | 85.2669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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