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 66842U 26145.42177771 +.00000000 +00000-0 +25277-3 0 00009
2 66842 70.0006 140.8251 0004118 264.7645 95.3044 14.98339056 03
| Epoch (UTC): | 25 May 2026 10:07:21 |
| Eccentricity: | 0.0004118 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.8251° |
| argument of perigee: | 264.7645° |
| revolutions per day: | 14.98339056 |
| mean anomaly at epoch: | 95.3044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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