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 58938U 26145.49483707 +.00000000 +00000-0 +98200-5 0 00000
2 58938 53.1617 313.1462 0001096 81.8551 278.2574 15.30189607 07
| Epoch (UTC): | 25 May 2026 11:52:33 |
| Eccentricity: | 0.0001096 |
| inclination: | 53.1617° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1462° |
| argument of perigee: | 81.8551° |
| revolutions per day: | 15.30189607 |
| mean anomaly at epoch: | 278.2574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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