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 58171U 26145.51293152 +.00000000 +00000-0 -87483-4 0 00006
2 58171 53.1600 222.6038 0001104 96.1184 263.9943 15.30200280 04
| Epoch (UTC): | 25 May 2026 12:18:37 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 222.6038° |
| argument of perigee: | 96.1184° |
| revolutions per day: | 15.30200280 |
| mean anomaly at epoch: | 263.9943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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