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 32258U 26113.34831468 +.00000000 +00000-0 +00000-0 0 00003
2 32258 0.0769 81.9874 0000708 234.9001 337.4084 1.00270335 05
| Epoch (UTC): | 23 April 2026 08:21:34 |
| Eccentricity: | 0.0000708 |
| inclination: | 0.0769° |
| perigee height: | 35784 km |
| apogee height: | 35790 km |
| right ascension of ascending node: | 81.9874° |
| argument of perigee: | 234.9001° |
| revolutions per day: | 1.00270335 |
| mean anomaly at epoch: | 337.4084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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