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 56392U 26145.26408024 +.00000000 +00000-0 +17398-4 0 00004
2 56392 43.0030 114.7628 0000985 248.0646 112.0102 15.27579646 07
| Epoch (UTC): | 25 May 2026 06:20:16 |
| Eccentricity: | 0.0000985 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.7628° |
| argument of perigee: | 248.0646° |
| revolutions per day: | 15.27579646 |
| mean anomaly at epoch: | 112.0102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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