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 66209U 26145.50235360 +.00000000 +00000-0 +43848-3 0 00008
2 66209 53.1616 232.8574 0000310 133.0544 227.0483 15.30190672 02
| Epoch (UTC): | 25 May 2026 12:03:23 |
| Eccentricity: | 0.0000310 |
| inclination: | 53.1616° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 232.8574° |
| argument of perigee: | 133.0544° |
| revolutions per day: | 15.30190672 |
| mean anomaly at epoch: | 227.0483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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