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 56408U 26145.35758875 +.00000000 +00000-0 +71794-5 0 00005
2 56408 43.0045 113.7241 0000987 262.3060 97.7680 15.27582943 06
| Epoch (UTC): | 25 May 2026 08:34:55 |
| Eccentricity: | 0.0000987 |
| inclination: | 43.0045° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 113.7241° |
| argument of perigee: | 262.3060° |
| revolutions per day: | 15.27582943 |
| mean anomaly at epoch: | 97.7680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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