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 43236U 26145.39127236 +.00000000 +00000-0 +49909-3 0 00006
2 43236 97.6338 314.5151 0002491 48.0279 312.1189 15.60295074 06
| Epoch (UTC): | 25 May 2026 09:23:25 |
| Eccentricity: | 0.0002491 |
| inclination: | 97.6338° |
| perigee height: | 385 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 314.5151° |
| argument of perigee: | 48.0279° |
| revolutions per day: | 15.60295074 |
| mean anomaly at epoch: | 312.1189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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