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 58447U 26145.51167308 +.00000000 +00000-0 +73184-4 0 00007
2 58447 43.0027 327.7647 0001735 262.0363 98.0292 15.27578700 02
| Epoch (UTC): | 25 May 2026 12:16:48 |
| Eccentricity: | 0.0001735 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.7647° |
| argument of perigee: | 262.0363° |
| revolutions per day: | 15.27578700 |
| mean anomaly at epoch: | 98.0292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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