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 58132U 26145.04392712 +.00000000 +00000-0 +13439-3 0 00001
2 58132 43.0012 61.3348 0001474 264.3099 95.7585 15.27573841 07
| Epoch (UTC): | 25 May 2026 01:03:15 |
| Eccentricity: | 0.0001474 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 61.3348° |
| argument of perigee: | 264.3099° |
| revolutions per day: | 15.27573841 |
| mean anomaly at epoch: | 95.7585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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