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 60588U 26145.47630725 +.00000000 +00000-0 +67218-4 0 00000
2 60588 53.1615 309.2331 0001174 93.1276 266.9861 15.34398829 02
| Epoch (UTC): | 25 May 2026 11:25:52 |
| Eccentricity: | 0.0001174 |
| inclination: | 53.1615° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 309.2331° |
| argument of perigee: | 93.1276° |
| revolutions per day: | 15.34398829 |
| mean anomaly at epoch: | 266.9861° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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