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 51962U 26145.38248860 +.00000000 +00000-0 +17743-3 0 00008
2 51962 53.1617 27.5926 0001317 102.6672 257.4477 15.31711186 05
| Epoch (UTC): | 25 May 2026 09:10:47 |
| Eccentricity: | 0.0001317 |
| inclination: | 53.1617° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 27.5926° |
| argument of perigee: | 102.6672° |
| revolutions per day: | 15.31711186 |
| mean anomaly at epoch: | 257.4477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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