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 58336U 26145.49921972 +.00000000 +00000-0 +44776-3 0 00000
2 58336 97.3904 235.3570 0005640 182.8858 177.2362 15.50373572 05
| Epoch (UTC): | 25 May 2026 11:58:52 |
| Eccentricity: | 0.0005640 |
| inclination: | 97.3904° |
| perigee height: | 412 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 235.3570° |
| argument of perigee: | 182.8858° |
| revolutions per day: | 15.50373572 |
| mean anomaly at epoch: | 177.2362° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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