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 43159U 26145.59571196 +.00000000 +00000-0 +25380-3 0 00007
2 43159 97.1786 166.1328 0009877 131.0872 229.1226 15.34287304 03
| Epoch (UTC): | 25 May 2026 14:17:49 |
| Eccentricity: | 0.0009877 |
| inclination: | 97.1786° |
| perigee height: | 456 km |
| apogee height: | 470 km |
| right ascension of ascending node: | 166.1328° |
| argument of perigee: | 131.0872° |
| revolutions per day: | 15.34287304 |
| mean anomaly at epoch: | 229.1226° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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