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 66607U 26145.57783987 +.00000000 +00000-0 +82112-3 0 00007
2 66607 42.9982 342.0639 0000425 310.8846 49.1969 15.27585728 07
| Epoch (UTC): | 25 May 2026 13:52:05 |
| Eccentricity: | 0.0000425 |
| inclination: | 42.9982° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 342.0639° |
| argument of perigee: | 310.8846° |
| revolutions per day: | 15.27585728 |
| mean anomaly at epoch: | 49.1969° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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