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 66256U 26145.64530390 +.00000000 +00000-0 +51084-3 0 00007
2 66256 53.1605 286.0897 0001437 91.5730 268.5436 15.30199938 09
| Epoch (UTC): | 25 May 2026 15:29:14 |
| Eccentricity: | 0.0001437 |
| inclination: | 53.1605° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.0897° |
| argument of perigee: | 91.5730° |
| revolutions per day: | 15.30199938 |
| mean anomaly at epoch: | 268.5436° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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