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 58020U 26145.50514705 +.00000000 +00000-0 +57526-3 0 00001
2 58020 97.5906 230.8107 0004556 274.9256 85.1464 15.29349843 05
| Epoch (UTC): | 25 May 2026 12:07:24 |
| Eccentricity: | 0.0004556 |
| inclination: | 97.5906° |
| perigee height: | 475 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 230.8107° |
| argument of perigee: | 274.9256° |
| revolutions per day: | 15.29349843 |
| mean anomaly at epoch: | 85.1464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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