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 60556U 26145.57700904 +.00000000 +00000-0 +62774-3 0 00004
2 60556 97.3731 231.8789 0000688 0.4276 359.6977 15.50893842 04
| Epoch (UTC): | 25 May 2026 13:50:53 |
| Eccentricity: | 0.0000688 |
| inclination: | 97.3731° |
| perigee height: | 414 km |
| apogee height: | 415 km |
| right ascension of ascending node: | 231.8789° |
| argument of perigee: | 0.4276° |
| revolutions per day: | 15.50893842 |
| mean anomaly at epoch: | 359.6977° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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