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 66192U 26145.26761491 +.00000000 +00000-0 +88337-3 0 00003
2 66192 53.1574 249.8820 0001220 93.7010 266.4130 15.30219761 06
| Epoch (UTC): | 25 May 2026 06:25:21 |
| Eccentricity: | 0.0001220 |
| inclination: | 53.1574° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 249.8820° |
| argument of perigee: | 93.7010° |
| revolutions per day: | 15.30219761 |
| mean anomaly at epoch: | 266.4130° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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