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 58453U 26145.50267747 +.00000000 +00000-0 +63115-4 0 00004
2 58453 43.0044 327.6706 0001921 273.0172 87.0460 15.27582697 05
| Epoch (UTC): | 25 May 2026 12:03:51 |
| Eccentricity: | 0.0001921 |
| inclination: | 43.0044° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.6706° |
| argument of perigee: | 273.0172° |
| revolutions per day: | 15.27582697 |
| mean anomaly at epoch: | 87.0460° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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