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 56012U 26145.54449626 +.00000000 +00000-0 +75429-5 0 00007
2 56012 43.0027 330.8403 0001012 246.1699 113.9047 15.27574505 00
| Epoch (UTC): | 25 May 2026 13:04:04 |
| Eccentricity: | 0.0001012 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 330.8403° |
| argument of perigee: | 246.1699° |
| revolutions per day: | 15.27574505 |
| mean anomaly at epoch: | 113.9047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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