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 58327U 26145.19975531 +.00000000 +00000-0 +40215-3 0 00001
2 58327 97.3821 232.4214 0005084 229.8652 130.2153 15.47515891 07
| Epoch (UTC): | 25 May 2026 04:47:38 |
| Eccentricity: | 0.0005084 |
| inclination: | 97.3821° |
| perigee height: | 421 km |
| apogee height: | 427 km |
| right ascension of ascending node: | 232.4214° |
| argument of perigee: | 229.8652° |
| revolutions per day: | 15.47515891 |
| mean anomaly at epoch: | 130.2153° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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