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 47590U 26145.63306498 +.00000000 +00000-0 +72614-3 0 00008
2 47590 53.0398 2.1317 0001561 122.9022 237.2146 15.71951911 05
| Epoch (UTC): | 25 May 2026 15:11:36 |
| Eccentricity: | 0.0001561 |
| inclination: | 53.0398° |
| perigee height: | 352 km |
| apogee height: | 354 km |
| right ascension of ascending node: | 2.1317° |
| argument of perigee: | 122.9022° |
| revolutions per day: | 15.71951911 |
| mean anomaly at epoch: | 237.2146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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