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 15032U 26039.47568528 +.00000000 +00000-0 +73803-4 0 00004
2 15032 74.0678 59.1348 0016108 148.6371 211.5747 14.36092007 00
| Epoch (UTC): | 08 February 2026 11:24:59 |
| Eccentricity: | 0.0016108 |
| inclination: | 74.0678° |
| perigee height: | 760 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 59.1348° |
| argument of perigee: | 148.6371° |
| revolutions per day: | 14.36092007 |
| mean anomaly at epoch: | 211.5747° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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