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 56381U 26145.63327580 +.00000000 +00000-0 -99458-4 0 00008
2 56381 43.0014 123.6642 0000633 262.5692 97.5088 15.27563058 04
| Epoch (UTC): | 25 May 2026 15:11:55 |
| Eccentricity: | 0.0000633 |
| inclination: | 43.0014° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 123.6642° |
| argument of perigee: | 262.5692° |
| revolutions per day: | 15.27563058 |
| mean anomaly at epoch: | 97.5088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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