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 65844U 26145.26144558 +.00000000 +00000-0 +10344-2 0 00007
2 65844 53.1595 92.1946 0001176 91.0696 269.0442 15.34406098 01
| Epoch (UTC): | 25 May 2026 06:16:28 |
| Eccentricity: | 0.0001176 |
| inclination: | 53.1595° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 92.1946° |
| argument of perigee: | 91.0696° |
| revolutions per day: | 15.34406098 |
| mean anomaly at epoch: | 269.0442° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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