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 66385U 26145.20986411 +.00000000 +00000-0 +84950-3 0 00009
2 66385 53.1592 220.5664 0001405 96.3778 263.7384 15.34427292 02
| Epoch (UTC): | 25 May 2026 05:02:12 |
| Eccentricity: | 0.0001405 |
| inclination: | 53.1592° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 220.5664° |
| argument of perigee: | 96.3778° |
| revolutions per day: | 15.34427292 |
| mean anomaly at epoch: | 263.7384° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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