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 58842U 26145.42650600 +.00000000 +00000-0 +46845-4 0 00002
2 58842 53.1608 207.9765 0001157 96.4623 263.6510 15.30191881 02
| Epoch (UTC): | 25 May 2026 10:14:10 |
| Eccentricity: | 0.0001157 |
| inclination: | 53.1608° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 207.9765° |
| argument of perigee: | 96.4623° |
| revolutions per day: | 15.30191881 |
| mean anomaly at epoch: | 263.6510° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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