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 66490U 26145.66157132 +.00000000 +00000-0 +61292-3 0 00000
2 66490 43.0026 275.7521 0000639 296.3128 63.7658 15.27594412 05
| Epoch (UTC): | 25 May 2026 15:52:39 |
| Eccentricity: | 0.0000639 |
| inclination: | 43.0026° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 275.7521° |
| argument of perigee: | 296.3128° |
| revolutions per day: | 15.27594412 |
| mean anomaly at epoch: | 63.7658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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