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 66040U 26145.64693625 +.00000000 +00000-0 +18340-3 0 00007
2 66040 89.0013 45.1971 0001911 84.8066 275.3303 13.51006841 02
| Epoch (UTC): | 25 May 2026 15:31:35 |
| Eccentricity: | 0.0001911 |
| inclination: | 89.0013° |
| perigee height: | 1067 km |
| apogee height: | 1070 km |
| right ascension of ascending node: | 45.1971° |
| argument of perigee: | 84.8066° |
| revolutions per day: | 13.51006841 |
| mean anomaly at epoch: | 275.3303° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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