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 01726U 26106.89534119 +.00000000 +00000-0 +17409-3 0 00008
2 01726 59.3793 166.8248 0716282 180.6524 352.5162 11.97076074 07
| Epoch (UTC): | 16 April 2026 21:29:17 |
| Eccentricity: | 0.0716282 |
| inclination: | 59.3793° |
| perigee height: | 1116 km |
| apogee height: | 2272 km |
| right ascension of ascending node: | 166.8248° |
| argument of perigee: | 180.6524° |
| revolutions per day: | 11.97076074 |
| mean anomaly at epoch: | 352.5162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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