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 47171U 26145.06302100 +.00000000 +00000-0 +68877-3 0 00002
2 47171 53.0469 269.5615 0002740 299.8578 60.2164 15.65263938 01
| Epoch (UTC): | 25 May 2026 01:30:45 |
| Eccentricity: | 0.0002740 |
| inclination: | 53.0469° |
| perigee height: | 371 km |
| apogee height: | 374 km |
| right ascension of ascending node: | 269.5615° |
| argument of perigee: | 299.8578° |
| revolutions per day: | 15.65263938 |
| mean anomaly at epoch: | 60.2164° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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