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 17192U 26067.72854855 +.00000000 +00000-0 +71196-4 0 00006
2 17192 82.5076 143.0647 0016924 32.9586 83.9825 14.85913310 00
| Epoch (UTC): | 08 March 2026 17:29:06 |
| Eccentricity: | 0.0016924 |
| inclination: | 82.5076° |
| perigee height: | 599 km |
| apogee height: | 623 km |
| right ascension of ascending node: | 143.0647° |
| argument of perigee: | 32.9586° |
| revolutions per day: | 14.85913310 |
| mean anomaly at epoch: | 83.9825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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