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 43170U 26145.64615838 +.00000000 +00000-0 +19923-3 0 00004
2 43170 34.9965 288.3308 0002721 140.5481 219.5426 15.02619852 08
| Epoch (UTC): | 25 May 2026 15:30:28 |
| Eccentricity: | 0.0002721 |
| inclination: | 34.9965° |
| perigee height: | 557 km |
| apogee height: | 561 km |
| right ascension of ascending node: | 288.3308° |
| argument of perigee: | 140.5481° |
| revolutions per day: | 15.02619852 |
| mean anomaly at epoch: | 219.5426° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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