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 43186U 26032.29063299 +.00000000 +00000-0 +30972-3 0 00002
2 43186 97.5477 297.9945 0009868 122.0361 238.1831 15.15116002 02
| Epoch (UTC): | 01 February 2026 06:58:30 |
| Eccentricity: | 0.0009868 |
| inclination: | 97.5477° |
| perigee height: | 514 km |
| apogee height: | 527 km |
| right ascension of ascending node: | 297.9945° |
| argument of perigee: | 122.0361° |
| revolutions per day: | 15.15116002 |
| mean anomaly at epoch: | 238.1831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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