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 18153U 26066.85939882 +.00000000 +00000-0 +92001-4 0 00009
2 18153 82.5030 350.7558 0021312 23.7418 336.4776 14.85627282 06
| Epoch (UTC): | 07 March 2026 20:37:32 |
| Eccentricity: | 0.0021312 |
| inclination: | 82.5030° |
| perigee height: | 597 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 350.7558° |
| argument of perigee: | 23.7418° |
| revolutions per day: | 14.85627282 |
| mean anomaly at epoch: | 336.4776° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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