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 26106.28799855 +.00000000 +00000-0 +16701-3 0 00005
2 01726 59.3793 168.1900 0716319 180.2544 255.1907 11.97076058 03
| Epoch (UTC): | 16 April 2026 06:54:43 |
| Eccentricity: | 0.0716319 |
| inclination: | 59.3793° |
| perigee height: | 1116 km |
| apogee height: | 2272 km |
| right ascension of ascending node: | 168.1900° |
| argument of perigee: | 180.2544° |
| revolutions per day: | 11.97076058 |
| mean anomaly at epoch: | 255.1907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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