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 59158U 26145.38557963 +.00000000 +00000-0 +22154-5 0 00004
2 59158 43.0032 34.0270 0001156 274.3702 85.7018 15.27581525 06
| Epoch (UTC): | 25 May 2026 09:15:14 |
| Eccentricity: | 0.0001156 |
| inclination: | 43.0032° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 34.0270° |
| argument of perigee: | 274.3702° |
| revolutions per day: | 15.27581525 |
| mean anomaly at epoch: | 85.7018° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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