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 66493U 26144.78598365 +.00000000 +00000-0 +28880-3 0 00008
2 66493 43.0002 281.2262 0003301 246.7950 113.2554 15.27578829 07
| Epoch (UTC): | 24 May 2026 18:51:48 |
| Eccentricity: | 0.0003301 |
| inclination: | 43.0002° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 281.2262° |
| argument of perigee: | 246.7950° |
| revolutions per day: | 15.27578829 |
| mean anomaly at epoch: | 113.2554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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