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 59657U 26145.52710829 +.00000000 +00000-0 +12293-4 0 00008
2 59657 43.0017 327.9334 0001299 274.2829 85.7874 15.27573668 04
| Epoch (UTC): | 25 May 2026 12:39:02 |
| Eccentricity: | 0.0001299 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.9334° |
| argument of perigee: | 274.2829° |
| revolutions per day: | 15.27573668 |
| mean anomaly at epoch: | 85.7874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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