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 66052U 26145.12944564 +.00000000 +00000-0 +49666-3 0 00009
2 66052 51.6268 37.3060 0003500 100.1879 259.9513 15.70522259 04
| Epoch (UTC): | 25 May 2026 03:06:24 |
| Eccentricity: | 0.0003500 |
| inclination: | 51.6268° |
| perigee height: | 355 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 37.3060° |
| argument of perigee: | 100.1879° |
| revolutions per day: | 15.70522259 |
| mean anomaly at epoch: | 259.9513° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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