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 56416U 26145.36876552 +.00000000 +00000-0 +18900-2 0 00005
2 56416 43.0033 106.7801 0002047 266.4947 93.5670 15.27316418 09
| Epoch (UTC): | 25 May 2026 08:51:01 |
| Eccentricity: | 0.0002047 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 106.7801° |
| argument of perigee: | 266.4947° |
| revolutions per day: | 15.27316418 |
| mean anomaly at epoch: | 93.5670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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