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 66223U 26145.54245216 +.00000000 +00000-0 +39194-3 0 00008
2 66223 53.1578 233.1056 0000494 88.8473 271.2584 15.30202044 05
| Epoch (UTC): | 25 May 2026 13:01:07 |
| Eccentricity: | 0.0000494 |
| inclination: | 53.1578° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 233.1056° |
| argument of perigee: | 88.8473° |
| revolutions per day: | 15.30202044 |
| mean anomaly at epoch: | 271.2584° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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