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 60356U 26145.17880318 +.00000000 +00000-0 +12240-4 0 00000
2 60356 53.1615 314.6505 0001117 99.3041 260.8086 15.30191377 00
| Epoch (UTC): | 25 May 2026 04:17:28 |
| Eccentricity: | 0.0001117 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 314.6505° |
| argument of perigee: | 99.3041° |
| revolutions per day: | 15.30191377 |
| mean anomaly at epoch: | 260.8086° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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