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 53183U 26145.43447499 +.00000000 +00000-0 -19680-3 0 00003
2 53183 53.2108 144.5125 0001116 70.4202 289.6910 15.08854230 08
| Epoch (UTC): | 25 May 2026 10:25:38 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 144.5125° |
| argument of perigee: | 70.4202° |
| revolutions per day: | 15.08854230 |
| mean anomaly at epoch: | 289.6910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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