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 66265U 26145.39144360 +.00000000 +00000-0 +19404-3 0 00007
2 66265 53.1593 193.9990 0000929 92.0577 268.0532 15.34394549 06
| Epoch (UTC): | 25 May 2026 09:23:40 |
| Eccentricity: | 0.0000929 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 193.9990° |
| argument of perigee: | 92.0577° |
| revolutions per day: | 15.34394549 |
| mean anomaly at epoch: | 268.0532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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