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 26152.24929610 +.00000000 +00000-0 -50872-4 0 00005
2 01726 59.3837 64.8740 0713814 210.3807 324.0814 11.97075929 09
| Epoch (UTC): | 01 June 2026 05:58:59 |
| Eccentricity: | 0.0713814 |
| inclination: | 59.3837° |
| perigee height: | 1118 km |
| apogee height: | 2270 km |
| right ascension of ascending node: | 64.8740° |
| argument of perigee: | 210.3807° |
| revolutions per day: | 11.97075929 |
| mean anomaly at epoch: | 324.0814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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