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 57182U 26145.57970266 +.00000000 +00000-0 +38817-3 0 00006
2 57182 97.5092 208.8370 0012228 172.4941 187.6483 15.27406618 05
| Epoch (UTC): | 25 May 2026 13:54:46 |
| Eccentricity: | 0.0012228 |
| inclination: | 97.5092° |
| perigee height: | 475 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 208.8370° |
| argument of perigee: | 172.4941° |
| revolutions per day: | 15.27406618 |
| mean anomaly at epoch: | 187.6483° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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