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 58375U 26145.58603434 +.00000000 +00000-0 +51780-4 0 00007
2 58375 53.1617 3.2591 0001160 97.7085 262.4050 15.34389704 00
| Epoch (UTC): | 25 May 2026 14:03:53 |
| Eccentricity: | 0.0001160 |
| inclination: | 53.1617° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 3.2591° |
| argument of perigee: | 97.7085° |
| revolutions per day: | 15.34389704 |
| mean anomaly at epoch: | 262.4050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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