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 59588U 26073.24987397 +.00000000 +00000-0 +19992-1 0 00006
2 59588 97.2038 13.3367 0064005 65.6555 295.1274 13.89829207 05
| Epoch (UTC): | 14 March 2026 05:59:49 |
| Eccentricity: | 0.0064005 |
| inclination: | 97.2038° |
| perigee height: | 882 km |
| apogee height: | 976 km |
| right ascension of ascending node: | 13.3367° |
| argument of perigee: | 65.6555° |
| revolutions per day: | 13.89829207 |
| mean anomaly at epoch: | 295.1274° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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