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 63732U 26145.39188250 +.00000000 +00000-0 +19343-3 0 00001
2 63732 51.8995 131.3933 0000556 67.5290 292.5732 14.80018538 06
| Epoch (UTC): | 25 May 2026 09:24:18 |
| Eccentricity: | 0.0000556 |
| inclination: | 51.8995° |
| perigee height: | 629 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 131.3933° |
| argument of perigee: | 67.5290° |
| revolutions per day: | 14.80018538 |
| mean anomaly at epoch: | 292.5732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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