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 60583U 26145.19558566 +.00000000 +00000-0 +12503-4 0 00003
2 60583 53.1608 311.0384 0001208 83.2525 276.8614 15.31704715 01
| Epoch (UTC): | 25 May 2026 04:41:38 |
| Eccentricity: | 0.0001208 |
| inclination: | 53.1608° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 311.0384° |
| argument of perigee: | 83.2525° |
| revolutions per day: | 15.31704715 |
| mean anomaly at epoch: | 276.8614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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