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 58182U 26145.50152666 +.00000000 +00000-0 +38171-4 0 00000
2 58182 43.0029 69.5022 0000619 291.9790 68.0996 15.27577416 04
| Epoch (UTC): | 25 May 2026 12:02:11 |
| Eccentricity: | 0.0000619 |
| inclination: | 43.0029° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 69.5022° |
| argument of perigee: | 291.9790° |
| revolutions per day: | 15.27577416 |
| mean anomaly at epoch: | 68.0996° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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