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 43152U 26145.57580749 +.00000000 +00000-0 +38525-3 0 00007
2 43152 97.3982 152.8555 0001722 92.8107 267.3327 15.22424981 03
| Epoch (UTC): | 25 May 2026 13:49:09 |
| Eccentricity: | 0.0001722 |
| inclination: | 97.3982° |
| perigee height: | 497 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 152.8555° |
| argument of perigee: | 92.8107° |
| revolutions per day: | 15.22424981 |
| mean anomaly at epoch: | 267.3327° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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