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 58621U 26145.30472530 +.00000000 +00000-0 -29496-4 0 00002
2 58621 43.0040 354.8428 0000208 261.8161 98.2667 15.27584724 07
| Epoch (UTC): | 25 May 2026 07:18:48 |
| Eccentricity: | 0.0000208 |
| inclination: | 43.0040° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 354.8428° |
| argument of perigee: | 261.8161° |
| revolutions per day: | 15.27584724 |
| mean anomaly at epoch: | 98.2667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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