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 09510U 26129.53055285 +.00000000 +00000-0 -22692-4 0 00007
2 09510 82.9340 126.1784 0027516 83.0962 277.3324 13.77886532 09
| Epoch (UTC): | 09 May 2026 12:43:59 |
| Eccentricity: | 0.0027516 |
| inclination: | 82.9340° |
| perigee height: | 951 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 126.1784° |
| argument of perigee: | 83.0962° |
| revolutions per day: | 13.77886532 |
| mean anomaly at epoch: | 277.3324° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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