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 59038U 26145.48447035 +.00000000 +00000-0 +29417-4 0 00008
2 59038 43.0009 309.8126 0000824 276.3712 83.7046 15.27575079 00
| Epoch (UTC): | 25 May 2026 11:37:38 |
| Eccentricity: | 0.0000824 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 309.8126° |
| argument of perigee: | 276.3712° |
| revolutions per day: | 15.27575079 |
| mean anomaly at epoch: | 83.7046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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