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 26071.16998958 +.00000000 +00000-0 +72557-4 0 00002
2 18153 82.5031 346.6945 0020955 9.7745 350.3874 14.85632826 04
| Epoch (UTC): | 12 March 2026 04:04:47 |
| Eccentricity: | 0.0020955 |
| inclination: | 82.5031° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 346.6945° |
| argument of perigee: | 9.7745° |
| revolutions per day: | 14.85632826 |
| mean anomaly at epoch: | 350.3874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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