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 58043U 26145.11912235 +.00000000 +00000-0 +11771-2 0 00004
2 58043 53.1564 83.4780 0001146 109.8291 250.2833 15.30188123 03
| Epoch (UTC): | 25 May 2026 02:51:32 |
| Eccentricity: | 0.0001146 |
| inclination: | 53.1564° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 83.4780° |
| argument of perigee: | 109.8291° |
| revolutions per day: | 15.30188123 |
| mean anomaly at epoch: | 250.2833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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