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 58464U 26145.62080735 +.00000000 +00000-0 +29719-3 0 00000
2 58464 97.5321 217.9550 0007513 37.3270 322.8484 15.17902513 08
| Epoch (UTC): | 25 May 2026 14:53:57 |
| Eccentricity: | 0.0007513 |
| inclination: | 97.5321° |
| perigee height: | 507 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 217.9550° |
| argument of perigee: | 37.3270° |
| revolutions per day: | 15.17902513 |
| mean anomaly at epoch: | 322.8484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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