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 52876U 26145.39906851 +.00000000 +00000-0 +26988-4 0 00007
2 52876 53.2130 29.7586 0001079 95.6197 264.4918 15.08840101 07
| Epoch (UTC): | 25 May 2026 09:34:39 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.2130° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 29.7586° |
| argument of perigee: | 95.6197° |
| revolutions per day: | 15.08840101 |
| mean anomaly at epoch: | 264.4918° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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