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 54201U 26145.03659110 +.00000000 +00000-0 +50092-5 0 00009
2 54201 53.2132 11.3828 0001560 95.4812 264.6358 15.08842230 01
| Epoch (UTC): | 25 May 2026 00:52:41 |
| Eccentricity: | 0.0001560 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 11.3828° |
| argument of perigee: | 95.4812° |
| revolutions per day: | 15.08842230 |
| mean anomaly at epoch: | 264.6358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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