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 44353U 26145.62046913 +.00000000 +00000-0 +16262-3 0 00001
2 44353 23.9967 121.7535 0001101 180.0486 180.0015 14.96396110 06
| Epoch (UTC): | 25 May 2026 14:53:28 |
| Eccentricity: | 0.0001101 |
| inclination: | 23.9967° |
| perigee height: | 577 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 121.7535° |
| argument of perigee: | 180.0486° |
| revolutions per day: | 14.96396110 |
| mean anomaly at epoch: | 180.0015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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