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 58481U 26145.52828242 +.00000000 +00000-0 +14770-3 0 00002
2 58481 43.0016 327.3342 0001312 273.0986 86.9716 15.27585481 01
| Epoch (UTC): | 25 May 2026 12:40:43 |
| Eccentricity: | 0.0001312 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.3342° |
| argument of perigee: | 273.0986° |
| revolutions per day: | 15.27585481 |
| mean anomaly at epoch: | 86.9716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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