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 53726U 26145.38433238 +.00000000 +00000-0 +46370-4 0 00002
2 53726 53.2132 269.6980 0001384 96.0990 264.0160 15.08839832 06
| Epoch (UTC): | 25 May 2026 09:13:26 |
| Eccentricity: | 0.0001384 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 269.6980° |
| argument of perigee: | 96.0990° |
| revolutions per day: | 15.08839832 |
| mean anomaly at epoch: | 264.0160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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