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 66082U 26145.27416137 +.00000000 +00000-0 +52210-3 0 00007
2 66082 53.1599 249.0583 0001066 91.3182 268.7941 15.31720992 00
| Epoch (UTC): | 25 May 2026 06:34:47 |
| Eccentricity: | 0.0001066 |
| inclination: | 53.1599° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 249.0583° |
| argument of perigee: | 91.3182° |
| revolutions per day: | 15.31720992 |
| mean anomaly at epoch: | 268.7941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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