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 57926U 26145.34887164 +.00000000 +00000-0 -70670-4 0 00006
2 57926 43.0018 255.5491 0001187 271.5548 88.5167 15.27583423 02
| Epoch (UTC): | 25 May 2026 08:22:22 |
| Eccentricity: | 0.0001187 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 255.5491° |
| argument of perigee: | 271.5548° |
| revolutions per day: | 15.27583423 |
| mean anomaly at epoch: | 88.5167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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