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 26067.26351740 +.00000000 +00000-0 +92715-4 0 00008
2 18153 82.5030 350.3750 0021277 22.4304 337.7837 14.85627974 06
| Epoch (UTC): | 08 March 2026 06:19:27 |
| Eccentricity: | 0.0021277 |
| inclination: | 82.5030° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 350.3750° |
| argument of perigee: | 22.4304° |
| revolutions per day: | 14.85627974 |
| mean anomaly at epoch: | 337.7837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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