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 55112U 26145.22069347 +.00000000 +00000-0 +74072-3 0 00001
2 55112 97.5650 238.9740 0008053 84.6839 275.5318 15.27606269 00
| Epoch (UTC): | 25 May 2026 05:17:47 |
| Eccentricity: | 0.0008053 |
| inclination: | 97.5650° |
| perigee height: | 477 km |
| apogee height: | 488 km |
| right ascension of ascending node: | 238.9740° |
| argument of perigee: | 84.6839° |
| revolutions per day: | 15.27606269 |
| mean anomaly at epoch: | 275.5318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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