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 56136U 26145.52670208 +.00000000 +00000-0 +57055-4 0 00008
2 56136 43.0055 72.8576 0001389 269.1267 90.9426 15.27579174 07
| Epoch (UTC): | 25 May 2026 12:38:27 |
| Eccentricity: | 0.0001389 |
| inclination: | 43.0055° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 72.8576° |
| argument of perigee: | 269.1267° |
| revolutions per day: | 15.27579174 |
| mean anomaly at epoch: | 90.9426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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