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 43260U 26145.64120512 +.00000000 +00000-0 +95673-4 0 00001
2 43260 98.0527 208.0905 0003472 129.1332 231.0187 14.76489757 09
| Epoch (UTC): | 25 May 2026 15:23:20 |
| Eccentricity: | 0.0003472 |
| inclination: | 98.0527° |
| perigee height: | 638 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 208.0905° |
| argument of perigee: | 129.1332° |
| revolutions per day: | 14.76489757 |
| mean anomaly at epoch: | 231.0187° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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