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 58296U 26144.83779347 +.00000000 +00000-0 +17358-3 0 00005
2 58296 97.4014 243.7390 0001374 52.2445 307.8943 15.72891035 07
| Epoch (UTC): | 24 May 2026 20:06:25 |
| Eccentricity: | 0.0001374 |
| inclination: | 97.4014° |
| perigee height: | 350 km |
| apogee height: | 352 km |
| right ascension of ascending node: | 243.7390° |
| argument of perigee: | 52.2445° |
| revolutions per day: | 15.72891035 |
| mean anomaly at epoch: | 307.8943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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