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 00011U 26158.57552757 +.00000000 +00000-0 +95346-3 0 00000
2 00011 32.8653 121.5359 1444589 2.1845 358.4285 11.90483764 00
| Epoch (UTC): | 07 June 2026 13:48:45 |
| Eccentricity: | 0.1444589 |
| inclination: | 32.8653° |
| perigee height: | 553 km |
| apogee height: | 2894 km |
| right ascension of ascending node: | 121.5359° |
| argument of perigee: | 2.1845° |
| revolutions per day: | 11.90483764 |
| mean anomaly at epoch: | 358.4285° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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