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 58861U 26145.12684323 +.00000000 +00000-0 +47623-5 0 00005
2 58861 43.0014 177.1465 0001507 267.9113 92.1566 15.27574730 05
| Epoch (UTC): | 25 May 2026 03:02:39 |
| Eccentricity: | 0.0001507 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 177.1465° |
| argument of perigee: | 267.9113° |
| revolutions per day: | 15.27574730 |
| mean anomaly at epoch: | 92.1566° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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