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 66985U 26145.18962737 +.00000000 +00000-0 +56446-3 0 00006
2 66985 43.0019 311.7154 0002577 272.8384 87.2173 15.27587552 05
| Epoch (UTC): | 25 May 2026 04:33:03 |
| Eccentricity: | 0.0002577 |
| inclination: | 43.0019° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 311.7154° |
| argument of perigee: | 272.8384° |
| revolutions per day: | 15.27587552 |
| mean anomaly at epoch: | 87.2173° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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