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 43146U 26145.62912865 +.00000000 +00000-0 +36251-3 0 00008
2 43146 97.6591 305.3343 0003641 48.0990 312.0562 15.34739687 04
| Epoch (UTC): | 25 May 2026 15:05:56 |
| Eccentricity: | 0.0003641 |
| inclination: | 97.6591° |
| perigee height: | 459 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 305.3343° |
| argument of perigee: | 48.0990° |
| revolutions per day: | 15.34739687 |
| mean anomaly at epoch: | 312.0562° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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