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 66193U 26145.55303686 +.00000000 +00000-0 +22316-3 0 00009
2 66193 53.1589 248.1055 0001710 86.4043 273.7153 15.30214887 04
| Epoch (UTC): | 25 May 2026 13:16:22 |
| Eccentricity: | 0.0001710 |
| inclination: | 53.1589° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 248.1055° |
| argument of perigee: | 86.4043° |
| revolutions per day: | 15.30214887 |
| mean anomaly at epoch: | 273.7153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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