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 66947U 26145.59385572 +.00000000 +00000-0 +85750-3 0 00005
2 66947 53.1604 1.0546 0001642 106.9314 253.1868 15.34411169 04
| Epoch (UTC): | 25 May 2026 14:15:09 |
| Eccentricity: | 0.0001642 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 1.0546° |
| argument of perigee: | 106.9314° |
| revolutions per day: | 15.34411169 |
| mean anomaly at epoch: | 253.1868° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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