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 65203U 26145.44892549 +.00000000 +00000-0 +54215-3 0 00002
2 65203 53.1576 155.4111 0001168 96.5794 263.5341 15.34408357 03
| Epoch (UTC): | 25 May 2026 10:46:27 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1576° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 155.4111° |
| argument of perigee: | 96.5794° |
| revolutions per day: | 15.34408357 |
| mean anomaly at epoch: | 263.5341° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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