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 55470U 26145.60021485 +.00000000 +00000-0 +19186-4 0 00007
2 55470 43.0008 254.4402 0000875 278.0534 82.0218 15.27575477 09
| Epoch (UTC): | 25 May 2026 14:24:18 |
| Eccentricity: | 0.0000875 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 254.4402° |
| argument of perigee: | 278.0534° |
| revolutions per day: | 15.27575477 |
| mean anomaly at epoch: | 82.0218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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