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 65605U 26145.52087317 +.00000000 +00000-0 -35390-2 0 00009
2 65605 97.4493 214.0424 0003245 175.5583 184.5673 15.05547598 08
| Epoch (UTC): | 25 May 2026 12:30:03 |
| Eccentricity: | 0.0003245 |
| inclination: | 97.4493° |
| perigee height: | 548 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 214.0424° |
| argument of perigee: | 175.5583° |
| revolutions per day: | 15.05547598 |
| mean anomaly at epoch: | 184.5673° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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