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 15399U 26160.28371889 +.00000000 +00000-0 +35793-4 0 00002
2 15399 82.9452 92.3949 0033566 351.0459 129.9720 13.76457001 09
| Epoch (UTC): | 09 June 2026 06:48:33 |
| Eccentricity: | 0.0033566 |
| inclination: | 82.9452° |
| perigee height: | 952 km |
| apogee height: | 1001 km |
| right ascension of ascending node: | 92.3949° |
| argument of perigee: | 351.0459° |
| revolutions per day: | 13.76457001 |
| mean anomaly at epoch: | 129.9720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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