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 66334U 26145.03646700 +.00000000 +00000-0 +47111-3 0 00006
2 66334 42.9984 141.0924 0000711 269.9297 90.1473 15.27596511 00
| Epoch (UTC): | 25 May 2026 00:52:30 |
| Eccentricity: | 0.0000711 |
| inclination: | 42.9984° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 141.0924° |
| argument of perigee: | 269.9297° |
| revolutions per day: | 15.27596511 |
| mean anomaly at epoch: | 90.1473° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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