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 56132U 26145.51642266 +.00000000 +00000-0 -34366-5 0 00008
2 56132 43.0056 72.7827 0001200 318.3600 41.7160 15.27588087 04
| Epoch (UTC): | 25 May 2026 12:23:38 |
| Eccentricity: | 0.0001200 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 72.7827° |
| argument of perigee: | 318.3600° |
| revolutions per day: | 15.27588087 |
| mean anomaly at epoch: | 41.7160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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