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 56395U 26145.21668632 +.00000000 +00000-0 -33144-4 0 00003
2 56395 43.0011 115.2648 0001239 270.7177 89.3533 15.27584100 06
| Epoch (UTC): | 25 May 2026 05:12:01 |
| Eccentricity: | 0.0001239 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 115.2648° |
| argument of perigee: | 270.7177° |
| revolutions per day: | 15.27584100 |
| mean anomaly at epoch: | 89.3533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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