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 17181U 26146.22868943 +.00000000 +00000-0 +00000-0 0 00002
2 17181 12.7192 340.2272 0041332 331.1169 31.0980 0.98929762 02
| Epoch (UTC): | 26 May 2026 05:29:18 |
| Eccentricity: | 0.0041332 |
| inclination: | 12.7192° |
| perigee height: | 35991 km |
| apogee height: | 36343 km |
| right ascension of ascending node: | 340.2272° |
| argument of perigee: | 331.1169° |
| revolutions per day: | 0.98929762 |
| mean anomaly at epoch: | 31.0980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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