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 59588U 26017.47790164 +.00000000 +00000-0 +69290-2 0 00000
2 59588 97.2374 330.0948 0056615 246.1757 113.3464 13.87220174 08
| Epoch (UTC): | 17 January 2026 11:28:10 |
| Eccentricity: | 0.0056615 |
| inclination: | 97.2374° |
| perigee height: | 897 km |
| apogee height: | 980 km |
| right ascension of ascending node: | 330.0948° |
| argument of perigee: | 246.1757° |
| revolutions per day: | 13.87220174 |
| mean anomaly at epoch: | 113.3464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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