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 66826U 26145.42161095 +.00000000 +00000-0 +14460-3 0 00005
2 66826 70.0006 140.8268 0004508 262.4022 97.6626 14.98339444 02
| Epoch (UTC): | 25 May 2026 10:07:07 |
| Eccentricity: | 0.0004508 |
| inclination: | 70.0006° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 140.8268° |
| argument of perigee: | 262.4022° |
| revolutions per day: | 14.98339444 |
| mean anomaly at epoch: | 97.6626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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