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 15332U 26039.69671131 +.00000000 +00000-0 +60174-4 0 00003
2 15332 82.5338 112.8052 0020735 29.0569 86.8612 14.85809738 06
| Epoch (UTC): | 08 February 2026 16:43:15 |
| Eccentricity: | 0.0020735 |
| inclination: | 82.5338° |
| perigee height: | 597 km |
| apogee height: | 626 km |
| right ascension of ascending node: | 112.8052° |
| argument of perigee: | 29.0569° |
| revolutions per day: | 14.85809738 |
| mean anomaly at epoch: | 86.8612° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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