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 27056U 26145.60957492 +.00000000 +00000-0 -34515-4 0 00006
2 27056 82.5376 234.2826 0004940 286.2091 208.6730 12.60564543 07
| Epoch (UTC): | 25 May 2026 14:37:47 |
| Eccentricity: | 0.0004940 |
| inclination: | 82.5376° |
| perigee height: | 1417 km |
| apogee height: | 1424 km |
| right ascension of ascending node: | 234.2826° |
| argument of perigee: | 286.2091° |
| revolutions per day: | 12.60564543 |
| mean anomaly at epoch: | 208.6730° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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