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 59672U 26145.52887458 +.00000000 +00000-0 +75544-4 0 00006
2 59672 43.0004 324.4783 0001109 268.9024 91.1700 15.27578091 08
| Epoch (UTC): | 25 May 2026 12:41:34 |
| Eccentricity: | 0.0001109 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.4783° |
| argument of perigee: | 268.9024° |
| revolutions per day: | 15.27578091 |
| mean anomaly at epoch: | 91.1700° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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