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 66864U 26040.31860437 +.00000000 +00000-0 +12339-2 0 00007
2 66864 42.9980 143.9453 0000867 269.8793 90.1959 15.27611055 04
| Epoch (UTC): | 09 February 2026 07:38:47 |
| Eccentricity: | 0.0000867 |
| inclination: | 42.9980° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 143.9453° |
| argument of perigee: | 269.8793° |
| revolutions per day: | 15.27611055 |
| mean anomaly at epoch: | 90.1959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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