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 56111U 26145.11088175 +.00000000 +00000-0 +14761-5 0 00000
2 56111 43.0056 90.4239 0001664 270.5239 89.5422 15.27573539 03
| Epoch (UTC): | 25 May 2026 02:39:40 |
| Eccentricity: | 0.0001664 |
| inclination: | 43.0056° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 90.4239° |
| argument of perigee: | 270.5239° |
| revolutions per day: | 15.27573539 |
| mean anomaly at epoch: | 89.5422° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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