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 58127U 26145.11521100 +.00000000 +00000-0 +13607-2 0 00004
2 58127 42.9991 63.6267 0015952 178.1506 181.9403 15.18083700 08
| Epoch (UTC): | 25 May 2026 02:45:54 |
| Eccentricity: | 0.0015952 |
| inclination: | 42.9991° |
| perigee height: | 501 km |
| apogee height: | 523 km |
| right ascension of ascending node: | 63.6267° |
| argument of perigee: | 178.1506° |
| revolutions per day: | 15.18083700 |
| mean anomaly at epoch: | 181.9403° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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