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 56116U 26144.97625426 +.00000000 +00000-0 +19762-4 0 00009
2 56116 43.0031 91.1548 0001547 275.0116 85.0559 15.27577036 04
| Epoch (UTC): | 24 May 2026 23:25:48 |
| Eccentricity: | 0.0001547 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 91.1548° |
| argument of perigee: | 275.0116° |
| revolutions per day: | 15.27577036 |
| mean anomaly at epoch: | 85.0559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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