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 56287U 26145.61753234 +.00000000 +00000-0 +56866-4 0 00005
2 56287 43.0018 116.7052 0000836 256.9557 103.1201 15.27578121 01
| Epoch (UTC): | 25 May 2026 14:49:14 |
| Eccentricity: | 0.0000836 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.7052° |
| argument of perigee: | 256.9557° |
| revolutions per day: | 15.27578121 |
| mean anomaly at epoch: | 103.1201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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