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 15392U 26162.43335999 +.00000000 +00000-0 +80186-5 0 00003
2 15392 21.4969 73.4229 1031965 211.1498 142.3520 12.46113151 03
| Epoch (UTC): | 11 June 2026 10:24:02 |
| Eccentricity: | 0.1031965 |
| inclination: | 21.4969° |
| perigee height: | 670 km |
| apogee height: | 2292 km |
| right ascension of ascending node: | 73.4229° |
| argument of perigee: | 211.1498° |
| revolutions per day: | 12.46113151 |
| mean anomaly at epoch: | 142.3520° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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