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 58981U 26145.40275304 +.00000000 +00000-0 +33440-4 0 00005
2 58981 53.1634 299.9888 0001412 96.1263 263.9901 15.34387493 00
| Epoch (UTC): | 25 May 2026 09:39:57 |
| Eccentricity: | 0.0001412 |
| inclination: | 53.1634° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 299.9888° |
| argument of perigee: | 96.1263° |
| revolutions per day: | 15.34387493 |
| mean anomaly at epoch: | 263.9901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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