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 59492U 26145.36208807 +.00000000 +00000-0 +15992-3 0 00003
2 59492 43.0011 274.3571 0001646 293.7895 66.2784 15.27592306 02
| Epoch (UTC): | 25 May 2026 08:41:24 |
| Eccentricity: | 0.0001646 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 274.3571° |
| argument of perigee: | 293.7895° |
| revolutions per day: | 15.27592306 |
| mean anomaly at epoch: | 66.2784° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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