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 17619U 26086.46675740 +.00000000 +00000-0 +14088-2 0 00001
2 17619 82.9375 85.6559 0017944 23.3750 129.5379 14.37083305 03
| Epoch (UTC): | 27 March 2026 11:12:07 |
| Eccentricity: | 0.0017944 |
| inclination: | 82.9375° |
| perigee height: | 755 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 85.6559° |
| argument of perigee: | 23.3750° |
| revolutions per day: | 14.37083305 |
| mean anomaly at epoch: | 129.5379° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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