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 26139.89194132 +.00000000 +00000-0 +32221-3 0 00009
2 43017 97.4738 7.6935 0153801 66.6401 295.0925 15.12149906 06
| Epoch (UTC): | 19 May 2026 21:24:23 |
| Eccentricity: | 0.0153801 |
| inclination: | 97.4738° |
| perigee height: | 423 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 7.6935° |
| argument of perigee: | 66.6401° |
| revolutions per day: | 15.12149906 |
| mean anomaly at epoch: | 295.0925° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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