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 26138.17988096 +.00000000 +00000-0 +00000-0 0 00009
2 17181 12.7256 340.2784 0041554 331.1942 44.4224 0.98926340 04
| Epoch (UTC): | 18 May 2026 04:19:01 |
| Eccentricity: | 0.0041554 |
| inclination: | 12.7256° |
| perigee height: | 35991 km |
| apogee height: | 36345 km |
| right ascension of ascending node: | 340.2784° |
| argument of perigee: | 331.1942° |
| revolutions per day: | 0.98926340 |
| mean anomaly at epoch: | 44.4224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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