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 58105U 26145.22726051 +.00000000 +00000-0 +12978-4 0 00006
2 58105 53.1625 156.8050 0001343 89.5464 270.5692 15.33546568 02
| Epoch (UTC): | 25 May 2026 05:27:15 |
| Eccentricity: | 0.0001343 |
| inclination: | 53.1625° |
| perigee height: | 464 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 156.8050° |
| argument of perigee: | 89.5464° |
| revolutions per day: | 15.33546568 |
| mean anomaly at epoch: | 270.5692° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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