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 56912U 26145.30423181 +.00000000 +00000-0 -22215-5 0 00004
2 56912 43.0046 358.1495 0001366 270.3071 89.7624 15.27575895 03
| Epoch (UTC): | 25 May 2026 07:18:05 |
| Eccentricity: | 0.0001366 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 358.1495° |
| argument of perigee: | 270.3071° |
| revolutions per day: | 15.27575895 |
| mean anomaly at epoch: | 89.7624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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