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 66926U 26145.32171611 +.00000000 +00000-0 +39034-3 0 00004
2 66926 53.1614 2.2062 0001039 94.5615 265.5506 15.33569652 00
| Epoch (UTC): | 25 May 2026 07:43:16 |
| Eccentricity: | 0.0001039 |
| inclination: | 53.1614° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 2.2062° |
| argument of perigee: | 94.5615° |
| revolutions per day: | 15.33569652 |
| mean anomaly at epoch: | 265.5506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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