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 66630U 26145.25925654 +.00000000 +00000-0 +68269-3 0 00004
2 66630 53.1593 142.5849 0000943 75.2295 284.8812 15.34405295 09
| Epoch (UTC): | 25 May 2026 06:13:19 |
| Eccentricity: | 0.0000943 |
| inclination: | 53.1593° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 142.5849° |
| argument of perigee: | 75.2295° |
| revolutions per day: | 15.34405295 |
| mean anomaly at epoch: | 284.8812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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