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 26065.51073700 +.00000000 +00000-0 +86676-4 0 00002
2 15392 21.4893 156.7339 1032031 138.1873 230.2160 12.46090579 01
| Epoch (UTC): | 06 March 2026 12:15:27 |
| Eccentricity: | 0.1032031 |
| inclination: | 21.4893° |
| perigee height: | 670 km |
| apogee height: | 2292 km |
| right ascension of ascending node: | 156.7339° |
| argument of perigee: | 138.1873° |
| revolutions per day: | 12.46090579 |
| mean anomaly at epoch: | 230.2160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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