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 66163U 26145.06899176 +.00000000 +00000-0 +12867-2 0 00005
2 66163 53.1589 67.2332 0001027 77.8049 282.3068 15.34443356 00
| Epoch (UTC): | 25 May 2026 01:39:20 |
| Eccentricity: | 0.0001027 |
| inclination: | 53.1589° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 67.2332° |
| argument of perigee: | 77.8049° |
| revolutions per day: | 15.34443356 |
| mean anomaly at epoch: | 282.3068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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