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 56732U 26145.60134345 +.00000000 +00000-0 +20485-3 0 00002
2 56732 41.0075 197.2883 0009445 91.6520 268.5375 15.10327623 01
| Epoch (UTC): | 25 May 2026 14:25:56 |
| Eccentricity: | 0.0009445 |
| inclination: | 41.0075° |
| perigee height: | 529 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 197.2883° |
| argument of perigee: | 91.6520° |
| revolutions per day: | 15.10327623 |
| mean anomaly at epoch: | 268.5375° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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