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 56966U 26145.55910248 +.00000000 +00000-0 +47596-3 0 00001
2 56966 97.5689 288.7000 0004839 339.3196 20.7855 15.44231726 03
| Epoch (UTC): | 25 May 2026 13:25:06 |
| Eccentricity: | 0.0004839 |
| inclination: | 97.5689° |
| perigee height: | 430 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 288.7000° |
| argument of perigee: | 339.3196° |
| revolutions per day: | 15.44231726 |
| mean anomaly at epoch: | 20.7855° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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