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 66836U 26145.43413720 +.00000000 +00000-0 +35703-3 0 00005
2 66836 70.0005 140.8700 0004189 263.7294 96.3388 14.98334851 01
| Epoch (UTC): | 25 May 2026 10:25:09 |
| Eccentricity: | 0.0004189 |
| inclination: | 70.0005° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.8700° |
| argument of perigee: | 263.7294° |
| revolutions per day: | 14.98334851 |
| mean anomaly at epoch: | 96.3388° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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