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 53876U 26145.92284727 +.00000000 +00000-0 +82547-3 0 00000
2 53876 28.9918 346.1795 0002566 44.2951 315.7863 15.43380030 07
| Epoch (UTC): | 25 May 2026 22:08:54 |
| Eccentricity: | 0.0002566 |
| inclination: | 28.9918° |
| perigee height: | 434 km |
| apogee height: | 438 km |
| right ascension of ascending node: | 346.1795° |
| argument of perigee: | 44.2951° |
| revolutions per day: | 15.43380030 |
| mean anomaly at epoch: | 315.7863° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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