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 66603U 26145.55086147 +.00000000 +00000-0 +70292-3 0 00001
2 66603 43.0018 341.8619 0002342 272.7791 87.2793 15.27581364 05
| Epoch (UTC): | 25 May 2026 13:13:14 |
| Eccentricity: | 0.0002342 |
| inclination: | 43.0018° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 341.8619° |
| argument of perigee: | 272.7791° |
| revolutions per day: | 15.27581364 |
| mean anomaly at epoch: | 87.2793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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