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 66134U 26145.41860895 +.00000000 +00000-0 +73597-2 0 00005
2 66134 53.1587 43.5342 0001265 150.0949 210.0124 15.30648840 03
| Epoch (UTC): | 25 May 2026 10:02:47 |
| Eccentricity: | 0.0001265 |
| inclination: | 53.1587° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 43.5342° |
| argument of perigee: | 150.0949° |
| revolutions per day: | 15.30648840 |
| mean anomaly at epoch: | 210.0124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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