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 66357U 26145.62519514 +.00000000 +00000-0 +57659-3 0 00006
2 66357 53.1591 235.1786 0001255 209.2220 150.8711 15.30216593 03
| Epoch (UTC): | 25 May 2026 15:00:16 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.1591° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 235.1786° |
| argument of perigee: | 209.2220° |
| revolutions per day: | 15.30216593 |
| mean anomaly at epoch: | 150.8711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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