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 66335U 26145.45063001 +.00000000 +00000-0 +50602-3 0 00009
2 66335 43.0020 139.0402 0001967 284.7490 75.3144 15.27588950 04
| Epoch (UTC): | 25 May 2026 10:48:54 |
| Eccentricity: | 0.0001967 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.0402° |
| argument of perigee: | 284.7490° |
| revolutions per day: | 15.27588950 |
| mean anomaly at epoch: | 75.3144° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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