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 58701U 26145.53997984 +.00000000 +00000-0 +20850-3 0 00004
2 58701 97.4622 330.9930 0007539 77.4776 282.7306 15.26475403 07
| Epoch (UTC): | 25 May 2026 12:57:34 |
| Eccentricity: | 0.0007539 |
| inclination: | 97.4622° |
| perigee height: | 481 km |
| apogee height: | 492 km |
| right ascension of ascending node: | 330.9930° |
| argument of perigee: | 77.4776° |
| revolutions per day: | 15.26475403 |
| mean anomaly at epoch: | 282.7306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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