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 58632U 26145.60161743 +.00000000 +00000-0 +25501-3 0 00009
2 58632 43.0008 356.2090 0001315 273.6396 86.4305 15.27588264 06
| Epoch (UTC): | 25 May 2026 14:26:19 |
| Eccentricity: | 0.0001315 |
| inclination: | 43.0008° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 356.2090° |
| argument of perigee: | 273.6396° |
| revolutions per day: | 15.27588264 |
| mean anomaly at epoch: | 86.4305° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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