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 58683U 26145.33963091 +.00000000 +00000-0 -22528-4 0 00009
2 58683 43.0059 12.7048 0001384 283.1999 76.8698 15.27565254 08
| Epoch (UTC): | 25 May 2026 08:09:04 |
| Eccentricity: | 0.0001384 |
| inclination: | 43.0059° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 12.7048° |
| argument of perigee: | 283.1999° |
| revolutions per day: | 15.27565254 |
| mean anomaly at epoch: | 76.8698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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