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 26069.21675501 +.00000000 +00000-0 +77508-4 0 00002
2 18153 82.5031 348.5347 0021120 16.0845 344.1037 14.85630376 08
| Epoch (UTC): | 10 March 2026 05:12:07 |
| Eccentricity: | 0.0021120 |
| inclination: | 82.5031° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 348.5347° |
| argument of perigee: | 16.0845° |
| revolutions per day: | 14.85630376 |
| mean anomaly at epoch: | 344.1037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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