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 66072U 26145.00421926 +.00000000 +00000-0 +53627-3 0 00002
2 66072 53.1577 250.9341 0000477 230.4400 129.6559 15.30217359 09
| Epoch (UTC): | 25 May 2026 00:06:04 |
| Eccentricity: | 0.0000477 |
| inclination: | 53.1577° |
| perigee height: | 475 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 250.9341° |
| argument of perigee: | 230.4400° |
| revolutions per day: | 15.30217359 |
| mean anomaly at epoch: | 129.6559° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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