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 58738U 26145.44199473 +.00000000 +00000-0 +30887-4 0 00003
2 58738 43.0043 146.1450 0001546 278.8472 81.2205 15.27578117 04
| Epoch (UTC): | 25 May 2026 10:36:28 |
| Eccentricity: | 0.0001546 |
| inclination: | 43.0043° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 146.1450° |
| argument of perigee: | 278.8472° |
| revolutions per day: | 15.27578117 |
| mean anomaly at epoch: | 81.2205° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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