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 59685U 26145.59533406 +.00000000 +00000-0 -15466-4 0 00006
2 59685 43.0023 345.5936 0001052 283.1287 76.9448 15.27573873 07
| Epoch (UTC): | 25 May 2026 14:17:16 |
| Eccentricity: | 0.0001052 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 345.5936° |
| argument of perigee: | 283.1287° |
| revolutions per day: | 15.27573873 |
| mean anomaly at epoch: | 76.9448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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