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 65932U 26145.33206294 +.00000000 +00000-0 +38477-3 0 00007
2 65932 53.1589 169.5903 0001096 75.7757 284.3365 15.30212007 07
| Epoch (UTC): | 25 May 2026 07:58:10 |
| Eccentricity: | 0.0001096 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 169.5903° |
| argument of perigee: | 75.7757° |
| revolutions per day: | 15.30212007 |
| mean anomaly at epoch: | 284.3365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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