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 43171U 26145.64103784 +.00000000 +00000-0 +20284-3 0 00009
2 43171 34.9956 288.1215 0000964 159.2585 200.8162 15.02590505 06
| Epoch (UTC): | 25 May 2026 15:23:05 |
| Eccentricity: | 0.0000964 |
| inclination: | 34.9956° |
| perigee height: | 558 km |
| apogee height: | 560 km |
| right ascension of ascending node: | 288.1215° |
| argument of perigee: | 159.2585° |
| revolutions per day: | 15.02590505 |
| mean anomaly at epoch: | 200.8162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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