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 43160U 26145.58189729 +.00000000 +00000-0 +18975-3 0 00007
2 43160 97.1816 165.4581 0007296 141.6397 218.5366 15.33382526 02
| Epoch (UTC): | 25 May 2026 13:57:55 |
| Eccentricity: | 0.0007296 |
| inclination: | 97.1816° |
| perigee height: | 461 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 165.4581° |
| argument of perigee: | 141.6397° |
| revolutions per day: | 15.33382526 |
| mean anomaly at epoch: | 218.5366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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