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 66638U 26145.37312457 +.00000000 +00000-0 +38611-3 0 00004
2 66638 53.1577 144.0005 0001018 90.1829 269.9288 15.30210809 05
| Epoch (UTC): | 25 May 2026 08:57:17 |
| Eccentricity: | 0.0001018 |
| inclination: | 53.1577° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 144.0005° |
| argument of perigee: | 90.1829° |
| revolutions per day: | 15.30210809 |
| mean anomaly at epoch: | 269.9288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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