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 56095U 26144.85689949 +.00000000 +00000-0 +25788-4 0 00007
2 56095 43.0052 91.1222 0001484 273.5783 86.4899 15.27579701 08
| Epoch (UTC): | 24 May 2026 20:33:56 |
| Eccentricity: | 0.0001484 |
| inclination: | 43.0052° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 91.1222° |
| argument of perigee: | 273.5783° |
| revolutions per day: | 15.27579701 |
| mean anomaly at epoch: | 86.4899° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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