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 43174U 26145.43714676 +.00000000 +00000-0 +00000-0 0 00008
2 43174 1.4954 83.3661 0004251 340.6275 316.3071 1.00272038 04
| Epoch (UTC): | 25 May 2026 10:29:29 |
| Eccentricity: | 0.0004251 |
| inclination: | 1.4954° |
| perigee height: | 35769 km |
| apogee height: | 35804 km |
| right ascension of ascending node: | 83.3661° |
| argument of perigee: | 340.6275° |
| revolutions per day: | 1.00272038 |
| mean anomaly at epoch: | 316.3071° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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