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 66614U 26145.59582463 +.00000000 +00000-0 +49269-3 0 00009
2 66614 42.9990 342.1974 0000603 165.6822 194.4046 15.27598606 04
| Epoch (UTC): | 25 May 2026 14:17:59 |
| Eccentricity: | 0.0000603 |
| inclination: | 42.9990° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 342.1974° |
| argument of perigee: | 165.6822° |
| revolutions per day: | 15.27598606 |
| mean anomaly at epoch: | 194.4046° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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