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 43017U 26138.56848332 +.00000000 +00000-0 +28271-3 0 00000
2 43017 97.4739 6.3981 0153828 71.1424 290.6416 15.12130594 08
| Epoch (UTC): | 18 May 2026 13:38:36 |
| Eccentricity: | 0.0153828 |
| inclination: | 97.4739° |
| perigee height: | 423 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 6.3981° |
| argument of perigee: | 71.1424° |
| revolutions per day: | 15.12130594 |
| mean anomaly at epoch: | 290.6416° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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