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 66173U 26145.59639674 +.00000000 +00000-0 +75809-3 0 00005
2 66173 53.1588 64.8369 0001301 105.8858 254.2288 15.34409420 04
| Epoch (UTC): | 25 May 2026 14:18:48 |
| Eccentricity: | 0.0001301 |
| inclination: | 53.1588° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 64.8369° |
| argument of perigee: | 105.8858° |
| revolutions per day: | 15.34409420 |
| mean anomaly at epoch: | 254.2288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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