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 57173U 26145.59539301 +.00000000 +00000-0 +41437-3 0 00001
2 57173 97.5062 208.6122 0010068 184.2220 175.8936 15.28063550 03
| Epoch (UTC): | 25 May 2026 14:17:21 |
| Eccentricity: | 0.0010068 |
| inclination: | 97.5062° |
| perigee height: | 475 km |
| apogee height: | 489 km |
| right ascension of ascending node: | 208.6122° |
| argument of perigee: | 184.2220° |
| revolutions per day: | 15.28063550 |
| mean anomaly at epoch: | 175.8936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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