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 66032U 26145.21848188 +.00000000 +00000-0 +19305-3 0 00009
2 66032 53.1613 108.3415 0001071 101.8856 258.2267 15.34405420 08
| Epoch (UTC): | 25 May 2026 05:14:36 |
| Eccentricity: | 0.0001071 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 108.3415° |
| argument of perigee: | 101.8856° |
| revolutions per day: | 15.34405420 |
| mean anomaly at epoch: | 258.2267° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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