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 62192U 26145.45537250 +.00000000 +00000-0 +45657-3 0 00002
2 62192 43.0033 193.5655 0001690 269.4502 90.6156 15.27587314 03
| Epoch (UTC): | 25 May 2026 10:55:44 |
| Eccentricity: | 0.0001690 |
| inclination: | 43.0033° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.5655° |
| argument of perigee: | 269.4502° |
| revolutions per day: | 15.27587314 |
| mean anomaly at epoch: | 90.6156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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