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 66012U 26145.19811838 +.00000000 +00000-0 +64973-3 0 00007
2 66012 53.1569 108.2288 0001345 90.3660 269.7494 15.30208495 00
| Epoch (UTC): | 25 May 2026 04:45:17 |
| Eccentricity: | 0.0001345 |
| inclination: | 53.1569° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 108.2288° |
| argument of perigee: | 90.3660° |
| revolutions per day: | 15.30208495 |
| mean anomaly at epoch: | 269.7494° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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