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 66247U 26145.40926301 +.00000000 +00000-0 +68609-3 0 00003
2 66247 53.1596 287.4680 0000783 50.7549 309.3522 15.31717887 01
| Epoch (UTC): | 25 May 2026 09:49:20 |
| Eccentricity: | 0.0000783 |
| inclination: | 53.1596° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 287.4680° |
| argument of perigee: | 50.7549° |
| revolutions per day: | 15.31717887 |
| mean anomaly at epoch: | 309.3522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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