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 66506U 26145.09236845 +.00000000 +00000-0 +54642-3 0 00005
2 66506 43.0007 279.2229 0002441 279.2442 80.8134 15.27586012 04
| Epoch (UTC): | 25 May 2026 02:13:00 |
| Eccentricity: | 0.0002441 |
| inclination: | 43.0007° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 279.2229° |
| argument of perigee: | 279.2442° |
| revolutions per day: | 15.27586012 |
| mean anomaly at epoch: | 80.8134° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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