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 66034U 26145.25609272 +.00000000 +00000-0 +17760-3 0 00007
2 66034 89.0002 45.4818 0002244 73.3397 286.8000 13.51008721 06
| Epoch (UTC): | 25 May 2026 06:08:46 |
| Eccentricity: | 0.0002244 |
| inclination: | 89.0002° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.4818° |
| argument of perigee: | 73.3397° |
| revolutions per day: | 13.51008721 |
| mean anomaly at epoch: | 286.8000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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