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 47270U 26145.32550422 +.00000000 +00000-0 +53838-3 0 00004
2 47270 87.8947 355.2202 0001862 84.0045 276.1295 13.12443390 04
| Epoch (UTC): | 25 May 2026 07:48:43 |
| Eccentricity: | 0.0001862 |
| inclination: | 87.8947° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2202° |
| argument of perigee: | 84.0045° |
| revolutions per day: | 13.12443390 |
| mean anomaly at epoch: | 276.1295° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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