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 47836U 26145.56275705 +.00000000 +00000-0 +27233-4 0 00007
2 47836 53.1581 247.4599 0001069 83.3176 276.7947 15.31703788 02
| Epoch (UTC): | 25 May 2026 13:30:22 |
| Eccentricity: | 0.0001069 |
| inclination: | 53.1581° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 247.4599° |
| argument of perigee: | 83.3176° |
| revolutions per day: | 15.31703788 |
| mean anomaly at epoch: | 276.7947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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