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 66174U 26100.01671284 +.00000000 +00000-0 +17113-3 0 00001
2 66174 51.6366 282.0284 0007351 294.6960 65.3256 15.32601237 08
| Epoch (UTC): | 10 April 2026 00:24:03 |
| Eccentricity: | 0.0007351 |
| inclination: | 51.6366° |
| perigee height: | 463 km |
| apogee height: | 473 km |
| right ascension of ascending node: | 282.0284° |
| argument of perigee: | 294.6960° |
| revolutions per day: | 15.32601237 |
| mean anomaly at epoch: | 65.3256° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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