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 66019U 26145.17395883 +.00000000 +00000-0 +62105-3 0 00004
2 66019 53.1591 108.7857 0001450 94.7098 265.4069 15.30214250 06
| Epoch (UTC): | 25 May 2026 04:10:30 |
| Eccentricity: | 0.0001450 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.7857° |
| argument of perigee: | 94.7098° |
| revolutions per day: | 15.30214250 |
| mean anomaly at epoch: | 265.4069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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