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 58288U 26145.63046036 +.00000000 +00000-0 +52366-3 0 00005
2 58288 97.3789 221.3914 0003213 73.7994 286.3602 15.33433259 01
| Epoch (UTC): | 25 May 2026 15:07:51 |
| Eccentricity: | 0.0003213 |
| inclination: | 97.3789° |
| perigee height: | 463 km |
| apogee height: | 468 km |
| right ascension of ascending node: | 221.3914° |
| argument of perigee: | 73.7994° |
| revolutions per day: | 15.33433259 |
| mean anomaly at epoch: | 286.3602° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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