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 53750U 26144.88665559 +.00000000 +00000-0 +50314-4 0 00009
2 53750 53.2118 282.2635 0001031 94.2806 265.8304 15.08835935 09
| Epoch (UTC): | 24 May 2026 21:16:47 |
| Eccentricity: | 0.0001031 |
| inclination: | 53.2118° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 282.2635° |
| argument of perigee: | 94.2806° |
| revolutions per day: | 15.08835935 |
| mean anomaly at epoch: | 265.8304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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