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 63833U 26145.66239990 +.00000000 +00000-0 +60584-3 0 00004
2 63833 97.3901 39.6193 0000756 341.9697 18.1516 15.29356441 04
| Epoch (UTC): | 25 May 2026 15:53:51 |
| Eccentricity: | 0.0000756 |
| inclination: | 97.3901° |
| perigee height: | 477 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 39.6193° |
| argument of perigee: | 341.9697° |
| revolutions per day: | 15.29356441 |
| mean anomaly at epoch: | 18.1516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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