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 55171U 26145.26265917 +.00000000 +00000-0 +98450-4 0 00008
2 55171 87.9167 339.9976 0001716 105.0698 255.0624 13.18687537 02
| Epoch (UTC): | 25 May 2026 06:18:13 |
| Eccentricity: | 0.0001716 |
| inclination: | 87.9167° |
| perigee height: | 1188 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 339.9976° |
| argument of perigee: | 105.0698° |
| revolutions per day: | 13.18687537 |
| mean anomaly at epoch: | 255.0624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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