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 66732U 26145.44122273 +.00000000 +00000-0 +26141-3 0 00007
2 66732 97.4177 219.2446 0005001 102.4675 257.7119 15.19425764 06
| Epoch (UTC): | 25 May 2026 10:35:21 |
| Eccentricity: | 0.0005001 |
| inclination: | 97.4177° |
| perigee height: | 504 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 219.2446° |
| argument of perigee: | 102.4675° |
| revolutions per day: | 15.19425764 |
| mean anomaly at epoch: | 257.7119° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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