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 66554U 26145.48343292 +.00000000 +00000-0 +27092-3 0 00005
2 66554 42.0184 188.3308 0007128 106.3713 253.7910 15.36123831 07
| Epoch (UTC): | 25 May 2026 11:36:08 |
| Eccentricity: | 0.0007128 |
| inclination: | 42.0184° |
| perigee height: | 453 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 188.3308° |
| argument of perigee: | 106.3713° |
| revolutions per day: | 15.36123831 |
| mean anomaly at epoch: | 253.7910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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