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 65171U 26145.58670256 +.00000000 +00000-0 +68400-4 0 00002
2 65171 86.4877 259.4570 0002023 94.6768 265.4597 13.24404440 05
| Epoch (UTC): | 25 May 2026 14:04:51 |
| Eccentricity: | 0.0002023 |
| inclination: | 86.4877° |
| perigee height: | 1166 km |
| apogee height: | 1169 km |
| right ascension of ascending node: | 259.4570° |
| argument of perigee: | 94.6768° |
| revolutions per day: | 13.24404440 |
| mean anomaly at epoch: | 265.4597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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