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 56957U 26145.48421652 +.00000000 +00000-0 +18123-3 0 00003
2 56957 98.1385 330.6651 0008504 113.4301 246.7831 15.28587491 03
| Epoch (UTC): | 25 May 2026 11:37:16 |
| Eccentricity: | 0.0008504 |
| inclination: | 98.1385° |
| perigee height: | 474 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 330.6651° |
| argument of perigee: | 113.4301° |
| revolutions per day: | 15.28587491 |
| mean anomaly at epoch: | 246.7831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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