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 66029U 26145.18345440 +.00000000 +00000-0 +70049-3 0 00006
2 66029 53.1570 108.8378 0001165 86.1723 273.9411 15.30211530 09
| Epoch (UTC): | 25 May 2026 04:24:10 |
| Eccentricity: | 0.0001165 |
| inclination: | 53.1570° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.8378° |
| argument of perigee: | 86.1723° |
| revolutions per day: | 15.30211530 |
| mean anomaly at epoch: | 273.9411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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