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 58873U 26145.57170698 +.00000000 +00000-0 +26726-3 0 00001
2 58873 42.9984 174.4593 0001595 275.7686 84.2984 15.27599231 02
| Epoch (UTC): | 25 May 2026 13:43:15 |
| Eccentricity: | 0.0001595 |
| inclination: | 42.9984° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 174.4593° |
| argument of perigee: | 275.7686° |
| revolutions per day: | 15.27599231 |
| mean anomaly at epoch: | 84.2984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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