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 58123U 26145.48620779 +.00000000 +00000-0 +12461-4 0 00001
2 58123 43.0065 58.6588 0001722 256.0438 104.0222 15.27586094 07
| Epoch (UTC): | 25 May 2026 11:40:08 |
| Eccentricity: | 0.0001722 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 58.6588° |
| argument of perigee: | 256.0438° |
| revolutions per day: | 15.27586094 |
| mean anomaly at epoch: | 104.0222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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