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 66327U 26145.36468684 +.00000000 +00000-0 +49615-3 0 00008
2 66327 43.0033 139.2551 0001637 262.6718 97.3947 15.27586532 07
| Epoch (UTC): | 25 May 2026 08:45:08 |
| Eccentricity: | 0.0001637 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 139.2551° |
| argument of perigee: | 262.6718° |
| revolutions per day: | 15.27586532 |
| mean anomaly at epoch: | 97.3947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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