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 66187U 26144.67450740 +.00000000 +00000-0 +31150-3 0 00004
2 66187 53.1564 252.5817 0000931 107.6517 252.4585 15.30202850 01
| Epoch (UTC): | 24 May 2026 16:11:17 |
| Eccentricity: | 0.0000931 |
| inclination: | 53.1564° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 252.5817° |
| argument of perigee: | 107.6517° |
| revolutions per day: | 15.30202850 |
| mean anomaly at epoch: | 252.4585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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