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 58148U 26145.63060303 +.00000000 +00000-0 +14128-3 0 00007
2 58148 67.1501 344.2519 0006535 278.7666 81.2678 13.96677074 09
| Epoch (UTC): | 25 May 2026 15:08:04 |
| Eccentricity: | 0.0006535 |
| inclination: | 67.1501° |
| perigee height: | 901 km |
| apogee height: | 910 km |
| right ascension of ascending node: | 344.2519° |
| argument of perigee: | 278.7666° |
| revolutions per day: | 13.96677074 |
| mean anomaly at epoch: | 81.2678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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