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 48056U 26145.50511549 +.00000000 +00000-0 +19040-3 0 00001
2 48056 87.8945 324.7421 0001934 94.5940 265.5410 13.13468158 00
| Epoch (UTC): | 25 May 2026 12:07:21 |
| Eccentricity: | 0.0001934 |
| inclination: | 87.8945° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7421° |
| argument of perigee: | 94.5940° |
| revolutions per day: | 13.13468158 |
| mean anomaly at epoch: | 265.5410° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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