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 58948U 26145.19927645 +.00000000 +00000-0 +41753-4 0 00002
2 58948 53.1610 312.0214 0001270 84.8125 275.3021 15.30194146 07
| Epoch (UTC): | 25 May 2026 04:46:57 |
| Eccentricity: | 0.0001270 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.0214° |
| argument of perigee: | 84.8125° |
| revolutions per day: | 15.30194146 |
| mean anomaly at epoch: | 275.3021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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